2000-03-22 22:01:33 +00:00
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/**********************************************************************
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FILENAME: uiuc_menu.cpp
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----------------------------------------------------------------------
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DESCRIPTION: reads input file for specified aircraft and creates
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approporiate data storage space
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----------------------------------------------------------------------
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STATUS: alpha version
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----------------------------------------------------------------------
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REFERENCES: based on "menu reader" format of Michael Selig
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----------------------------------------------------------------------
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HISTORY: 01/29/2000 initial release
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02/18/2000 (JS) added 1D data file capability for
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CL(a) and CD(a) -- calls
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uiuc_1DdataFileReader
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02/22/2000 (JS) added ice map functions
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02/29/2000 (JS) added 2D data file capability for
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CL(a,de), CD(a,de), Cm(a,de), CY(a,da),
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CY(beta,dr), Cl(a,da), Cl(beta,dr),
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Cn(a,da), Cn(beta,dr) -- calls
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uiuc_2DdataFileReader
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02/02/2000 (JS) added record options for 1D and
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2D interpolated variables
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2000-09-06 19:52:37 +00:00
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03/28/2000 (JS) streamlined conversion factors for
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file readers -- since they are global
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variables, it is not necessary to put
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them in the function calls
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03/29/2000 (JS) added Cmfa and Weight flags;
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added misc map; added Dx_cg (etc) to init
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map
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04/01/2000 (JS) added throttle, longitudinal, lateral,
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and rudder inputs to record map
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04/05/2000 (JS) added Altitude to init and record
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maps; added zero_Long_trim to
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controlSurface map
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From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
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03/09/2001 (DPM) added support for gear.
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2001-09-14 20:36:34 +00:00
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06/18/2001 (RD) Added Alpha, Beta, U_body,
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V_body, and W_body to init map. Added
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aileron_input, rudder_input, pilot_elev_no,
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pilot_ail_no, and pilot_rud_no to
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controlSurface map. Added Throttle_pct_input
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to engine map. Added CZfa to CL map.
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07/05/2001 (RD) Changed pilot_elev_no = true to pilot_
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elev_no_check=false. This is to allow pilot
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to fly aircraft after input files have been
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used.
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08/27/2001 (RD) Added xxx_init_true and xxx_init for
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P_body, Q_body, R_body, Phi, Theta, Psi,
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U_body, V_body, and W_body to help in
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starting the A/C at an initial condition.
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2002-04-01 21:37:33 +00:00
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10/25/2001 (RD) Added new variables needed for the non-
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linear Twin Otter model at zero flaps
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(Cxfxxf0)
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11/12/2001 (RD) Added new variables needed for the non-
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linear Twin Otter model with flaps
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(Cxfxxf). Removed zero flap variables.
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Added minmaxfind() which is needed for non-
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linear variables
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02/13/2002 (RD) Added variables so linear aero model
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values can be recorded
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02/18/2002 (RD) Added variables necessary to use the
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uiuc_3Dinterp_quick() function. Takes
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advantage of data in a "nice" form (data
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that are in a rectangular matrix).
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03/13/2002 (RD) Added aircraft_directory so full path
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is no longer needed in the aircraft.dat file
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2000-03-22 22:01:33 +00:00
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----------------------------------------------------------------------
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AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>
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Jeff Scott <jscott@mail.com>
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2001-09-14 20:36:34 +00:00
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Robert Deters <rdeters@uiuc.edu>
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2000-03-22 22:01:33 +00:00
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Michael Selig <m-selig@uiuc.edu>
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From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
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David Megginson <david@megginson.com>
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2000-03-22 22:01:33 +00:00
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----------------------------------------------------------------------
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VARIABLES:
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----------------------------------------------------------------------
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INPUTS: n/a
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----------------------------------------------------------------------
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OUTPUTS: n/a
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----------------------------------------------------------------------
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2000-09-06 19:52:37 +00:00
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CALLED BY: uiuc_wrapper.cpp
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2000-03-22 22:01:33 +00:00
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----------------------------------------------------------------------
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CALLS TO: aircraft.dat
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tabulated data files (if needed)
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----------------------------------------------------------------------
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COPYRIGHT: (C) 2000 by Michael Selig
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This program is free software; you can redistribute it and/or
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modify it under the terms of the GNU General Public License
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as published by the Free Software Foundation.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program; if not, write to the Free Software
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Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307,
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USA or view http://www.gnu.org/copyleft/gpl.html.
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**********************************************************************/
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2000-10-02 21:49:04 +00:00
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#include <simgear/compiler.h>
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2000-12-13 23:02:02 +00:00
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#if defined( __MWERKS__ )
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// -dw- optimizer chokes (big-time) trying to optimize humongous
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// loop/switch statements
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#pragma optimization_level 0
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#endif
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#include <stdlib.h>
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From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
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|
|
#include STL_IOSTREAM
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2000-10-02 21:49:04 +00:00
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2000-12-13 23:02:02 +00:00
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#include "uiuc_menu.h"
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2001-04-13 21:00:07 +00:00
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#if !defined (SG_HAVE_NATIVE_SGI_COMPILERS)
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2001-03-23 22:59:18 +00:00
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SG_USING_STD(cerr);
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SG_USING_STD(cout);
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SG_USING_STD(endl);
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2001-01-11 04:54:33 +00:00
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2001-05-17 21:55:22 +00:00
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# ifndef _MSC_VER
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2001-03-23 22:59:18 +00:00
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SG_USING_STD(exit);
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2001-04-13 21:00:07 +00:00
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# endif
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2001-01-11 04:54:33 +00:00
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#endif
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2000-03-22 22:01:33 +00:00
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bool check_float(string &token)
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{
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2000-09-06 19:52:37 +00:00
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float value;
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istrstream stream(token.c_str());
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return (stream >> value);
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2000-03-22 22:01:33 +00:00
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}
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|
2002-04-01 21:37:33 +00:00
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void minmaxfind( bool tarray[30], int &tmin, int &tmax)
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{
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int n=0;
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bool first=true;
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while (n<=30)
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{
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if (tarray[n])
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{
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if (first)
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{
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tmin=n;
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first=false;
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}
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tmax=n;
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}
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n++;
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}
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}
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2000-03-22 22:01:33 +00:00
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|
2000-09-06 19:52:37 +00:00
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|
void uiuc_menu( string aircraft_name )
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2000-03-22 22:01:33 +00:00
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{
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2002-04-01 21:37:33 +00:00
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|
|
string aircraft_directory;
|
2000-03-22 22:01:33 +00:00
|
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|
stack command_list;
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|
double token_value;
|
2000-09-06 19:52:37 +00:00
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|
|
int token_value_recordRate;
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|
int token_value_convert1, token_value_convert2, token_value_convert3;
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2000-03-22 22:01:33 +00:00
|
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|
string linetoken1;
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|
string linetoken2;
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|
string linetoken3;
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|
string linetoken4;
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|
string linetoken5;
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|
|
string linetoken6;
|
2002-04-01 21:37:33 +00:00
|
|
|
string linetoken7;
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|
|
string linetoken8;
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|
|
string linetoken9;
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|
|
|
|
|
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|
|
double datafile_xArray[100][100], datafile_yArray[100];
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|
|
double datafile_zArray[100][100];
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|
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|
|
int datafile_nxArray[100], datafile_ny;
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|
|
bool CXfabetaf_first = true;
|
|
|
|
|
bool CXfadef_first = true;
|
|
|
|
|
bool CXfaqf_first = true;
|
|
|
|
|
bool CZfabetaf_first = true;
|
|
|
|
|
bool CZfadef_first = true;
|
|
|
|
|
bool CZfaqf_first = true;
|
|
|
|
|
bool Cmfabetaf_first = true;
|
|
|
|
|
bool Cmfadef_first = true;
|
|
|
|
|
bool Cmfaqf_first = true;
|
|
|
|
|
bool CYfabetaf_first = true;
|
|
|
|
|
bool CYfadaf_first = true;
|
|
|
|
|
bool CYfadrf_first = true;
|
|
|
|
|
bool CYfapf_first = true;
|
|
|
|
|
bool CYfarf_first = true;
|
|
|
|
|
bool Clfabetaf_first = true;
|
|
|
|
|
bool Clfadaf_first = true;
|
|
|
|
|
bool Clfadrf_first = true;
|
|
|
|
|
bool Clfapf_first = true;
|
|
|
|
|
bool Clfarf_first = true;
|
|
|
|
|
bool Cnfabetaf_first = true;
|
|
|
|
|
bool Cnfadaf_first = true;
|
|
|
|
|
bool Cnfadrf_first = true;
|
|
|
|
|
bool Cnfapf_first = true;
|
|
|
|
|
bool Cnfarf_first = true;
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
/* the following default setting should eventually be moved to a default or uiuc_init routine */
|
|
|
|
|
|
|
|
|
|
recordRate = 1; /* record every time step, default */
|
|
|
|
|
recordStartTime = 0; /* record from beginning of simulation */
|
|
|
|
|
|
|
|
|
|
/* set speed at which dynamic pressure terms will be accounted for,
|
|
|
|
|
since if velocity is too small, coefficients will go to infinity */
|
|
|
|
|
dyn_on_speed = 33; /* 20 kts, default */
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
/* Read the file and get the list of commands */
|
|
|
|
|
airplane = new ParseFile(aircraft_name); /* struct that includes all lines of the input file */
|
|
|
|
|
command_list = airplane -> getCommands();
|
|
|
|
|
/* structs to include all parts included in the input file for specific keyword groups */
|
2000-09-06 19:52:37 +00:00
|
|
|
initParts = new ParseFile();
|
|
|
|
|
geometryParts = new ParseFile();
|
|
|
|
|
massParts = new ParseFile();
|
|
|
|
|
engineParts = new ParseFile();
|
|
|
|
|
aeroDragParts = new ParseFile();
|
|
|
|
|
aeroLiftParts = new ParseFile();
|
|
|
|
|
aeroPitchParts = new ParseFile();
|
|
|
|
|
aeroSideforceParts = new ParseFile();
|
|
|
|
|
aeroRollParts = new ParseFile();
|
|
|
|
|
aeroYawParts = new ParseFile();
|
|
|
|
|
gearParts = new ParseFile();
|
|
|
|
|
recordParts = new ParseFile();
|
2000-03-22 22:01:33 +00:00
|
|
|
|
|
|
|
|
if (command_list.begin() == command_list.end())
|
|
|
|
|
{
|
|
|
|
|
cerr << "UIUC ERROR: File " << aircraft_name <<" does not exist" << endl;
|
|
|
|
|
exit(-1);
|
|
|
|
|
}
|
|
|
|
|
|
2002-04-01 21:37:33 +00:00
|
|
|
cerr << "UIUC File " << aircraft_name <<" is being used" << endl;
|
|
|
|
|
aircraft_directory = aircraft_name;
|
|
|
|
|
int index_aircraft_dat = aircraft_directory.find("aircraft.dat");
|
|
|
|
|
aircraft_directory.erase(index_aircraft_dat,12);
|
|
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
for (LIST command_line = command_list.begin(); command_line!=command_list.end(); ++command_line)
|
|
|
|
|
{
|
|
|
|
|
cout << *command_line << endl;
|
2000-09-06 19:52:37 +00:00
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
linetoken1 = airplane -> getToken (*command_line, 1);
|
|
|
|
|
linetoken2 = airplane -> getToken (*command_line, 2);
|
|
|
|
|
linetoken3 = airplane -> getToken (*command_line, 3);
|
|
|
|
|
linetoken4 = airplane -> getToken (*command_line, 4);
|
|
|
|
|
linetoken5 = airplane -> getToken (*command_line, 5);
|
|
|
|
|
linetoken6 = airplane -> getToken (*command_line, 6);
|
2002-04-01 21:37:33 +00:00
|
|
|
linetoken7 = airplane -> getToken (*command_line, 7);
|
|
|
|
|
linetoken8 = airplane -> getToken (*command_line, 8);
|
|
|
|
|
linetoken9 = airplane -> getToken (*command_line, 9);
|
2000-03-22 22:01:33 +00:00
|
|
|
|
|
|
|
|
istrstream token3(linetoken3.c_str());
|
|
|
|
|
istrstream token4(linetoken4.c_str());
|
|
|
|
|
istrstream token5(linetoken5.c_str());
|
|
|
|
|
istrstream token6(linetoken6.c_str());
|
2002-04-01 21:37:33 +00:00
|
|
|
istrstream token7(linetoken7.c_str());
|
|
|
|
|
istrstream token8(linetoken8.c_str());
|
|
|
|
|
istrstream token9(linetoken9.c_str());
|
2000-03-22 22:01:33 +00:00
|
|
|
|
|
|
|
|
switch (Keyword_map[linetoken1])
|
|
|
|
|
{
|
|
|
|
|
case init_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(init_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case Dx_pilot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Dx_pilot = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dy_pilot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Dy_pilot = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dz_pilot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Dz_pilot = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Dx_cg_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Dx_cg = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dy_cg_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Dy_cg = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dz_cg_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Dz_cg = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Altitude_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Altitude = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
case V_north_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
V_north = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_east_flag:
|
|
|
|
|
{
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
V_east = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_down_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
V_down = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case P_body_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
2001-09-14 20:36:34 +00:00
|
|
|
|
|
|
|
|
P_body_init_true = true;
|
|
|
|
|
P_body_init = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Q_body_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2001-09-14 20:36:34 +00:00
|
|
|
Q_body_init_true = true;
|
|
|
|
|
Q_body_init = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case R_body_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2001-09-14 20:36:34 +00:00
|
|
|
R_body_init_true = true;
|
|
|
|
|
R_body_init = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Phi_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2001-09-14 20:36:34 +00:00
|
|
|
Phi_init_true = true;
|
|
|
|
|
Phi_init = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Theta_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2001-09-14 20:36:34 +00:00
|
|
|
Theta_init_true = true;
|
|
|
|
|
Theta_init = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Psi_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2001-09-14 20:36:34 +00:00
|
|
|
Psi_init_true = true;
|
|
|
|
|
Psi_init = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Long_trim_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Long_trim = token_value;
|
|
|
|
|
initParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case recordRate_flag:
|
|
|
|
|
{
|
|
|
|
|
//can't use check_float since variable is integer
|
|
|
|
|
token3 >> token_value_recordRate;
|
|
|
|
|
recordRate = 120 / token_value_recordRate;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case recordStartTime_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
recordStartTime = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case nondim_rate_V_rel_wind_flag:
|
|
|
|
|
{
|
|
|
|
|
nondim_rate_V_rel_wind = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case dyn_on_speed_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
dyn_on_speed = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2001-09-14 20:36:34 +00:00
|
|
|
case Alpha_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Alpha_init_true = true;
|
|
|
|
|
Alpha_init = token_value * DEG_TO_RAD;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Beta_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Beta_init_true = true;
|
|
|
|
|
Beta_init = token_value * DEG_TO_RAD;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case U_body_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
U_body_init_true = true;
|
|
|
|
|
U_body_init = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_body_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
V_body_init_true = true;
|
|
|
|
|
V_body_init = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case W_body_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
W_body_init_true = true;
|
|
|
|
|
W_body_init = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end init map
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
case geometry_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(geometry_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case bw_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
bw = token_value;
|
|
|
|
|
geometryParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case cbar_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
cbar = token_value;
|
|
|
|
|
geometryParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Sw_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Sw = token_value;
|
|
|
|
|
geometryParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case ih_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
ih = token_value;
|
|
|
|
|
geometryParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case bh_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
bh = token_value;
|
|
|
|
|
geometryParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case ch_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
ch = token_value;
|
|
|
|
|
geometryParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Sh_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Sh = token_value;
|
|
|
|
|
geometryParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end geometry map
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
case controlSurface_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(controlSurface_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
demax = token_value;
|
|
|
|
|
|
|
|
|
|
if (check_float(linetoken4))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
demin = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case da_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
damax = token_value;
|
|
|
|
|
|
|
|
|
|
if (check_float(linetoken4))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
damin = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
drmax = token_value;
|
|
|
|
|
|
|
|
|
|
if (check_float(linetoken4))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
drmin = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case set_Long_trim_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
set_Long_trim = true;
|
|
|
|
|
elevator_tab = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case set_Long_trim_deg_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
set_Long_trim = true;
|
|
|
|
|
elevator_tab = token_value * DEG_TO_RAD;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case zero_Long_trim_flag:
|
|
|
|
|
{
|
|
|
|
|
zero_Long_trim = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case elevator_step_flag:
|
|
|
|
|
{
|
|
|
|
|
// set step input flag
|
|
|
|
|
elevator_step = true;
|
|
|
|
|
|
|
|
|
|
// read in step angle in degrees and convert
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
elevator_step_angle = token_value * DEG_TO_RAD;
|
|
|
|
|
|
|
|
|
|
// read in step start time
|
|
|
|
|
if (check_float(linetoken4))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
elevator_step_startTime = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case elevator_singlet_flag:
|
|
|
|
|
{
|
|
|
|
|
// set singlet input flag
|
|
|
|
|
elevator_singlet = true;
|
|
|
|
|
|
|
|
|
|
// read in singlet angle in degrees and convert
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
elevator_singlet_angle = token_value * DEG_TO_RAD;
|
|
|
|
|
|
|
|
|
|
// read in singlet start time
|
|
|
|
|
if (check_float(linetoken4))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
elevator_singlet_startTime = token_value;
|
|
|
|
|
|
|
|
|
|
// read in singlet duration
|
|
|
|
|
if (check_float(linetoken5))
|
|
|
|
|
token5 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
elevator_singlet_duration = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case elevator_doublet_flag:
|
|
|
|
|
{
|
|
|
|
|
// set doublet input flag
|
|
|
|
|
elevator_doublet = true;
|
|
|
|
|
|
|
|
|
|
// read in doublet angle in degrees and convert
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
elevator_doublet_angle = token_value * DEG_TO_RAD;
|
|
|
|
|
|
|
|
|
|
// read in doublet start time
|
|
|
|
|
if (check_float(linetoken4))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
elevator_doublet_startTime = token_value;
|
|
|
|
|
|
|
|
|
|
// read in doublet duration
|
|
|
|
|
if (check_float(linetoken5))
|
|
|
|
|
token5 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
elevator_doublet_duration = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case elevator_input_flag:
|
|
|
|
|
{
|
|
|
|
|
elevator_input = true;
|
2002-04-01 21:37:33 +00:00
|
|
|
elevator_input_file = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
uiuc_1DdataFileReader(elevator_input_file,
|
|
|
|
|
elevator_input_timeArray,
|
|
|
|
|
elevator_input_deArray,
|
|
|
|
|
elevator_input_ntime);
|
|
|
|
|
token6 >> token_value;
|
|
|
|
|
elevator_input_startTime = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2001-09-14 20:36:34 +00:00
|
|
|
case aileron_input_flag:
|
|
|
|
|
{
|
|
|
|
|
aileron_input = true;
|
2002-04-01 21:37:33 +00:00
|
|
|
aileron_input_file = aircraft_directory + linetoken3;
|
2001-09-14 20:36:34 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
uiuc_1DdataFileReader(aileron_input_file,
|
|
|
|
|
aileron_input_timeArray,
|
|
|
|
|
aileron_input_daArray,
|
|
|
|
|
aileron_input_ntime);
|
|
|
|
|
token6 >> token_value;
|
|
|
|
|
aileron_input_startTime = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case rudder_input_flag:
|
|
|
|
|
{
|
|
|
|
|
rudder_input = true;
|
2002-04-01 21:37:33 +00:00
|
|
|
rudder_input_file = aircraft_directory + linetoken3;
|
2001-09-14 20:36:34 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
uiuc_1DdataFileReader(rudder_input_file,
|
|
|
|
|
rudder_input_timeArray,
|
|
|
|
|
rudder_input_drArray,
|
|
|
|
|
rudder_input_ntime);
|
|
|
|
|
token6 >> token_value;
|
|
|
|
|
rudder_input_startTime = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case pilot_elev_no_flag:
|
|
|
|
|
{
|
|
|
|
|
pilot_elev_no_check = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case pilot_ail_no_flag:
|
|
|
|
|
{
|
|
|
|
|
pilot_ail_no_check = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case pilot_rud_no_flag:
|
|
|
|
|
{
|
|
|
|
|
pilot_rud_no_check = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case flap_max_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
flap_max = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case flap_rate_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
flap_rate = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end controlSurface map
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
case mass_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(mass_map[linetoken2])
|
|
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
case Weight_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Weight = token_value;
|
|
|
|
|
Mass = Weight * INVG;
|
|
|
|
|
massParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
case Mass_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Mass = token_value;
|
|
|
|
|
massParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case I_xx_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
I_xx = token_value;
|
|
|
|
|
massParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case I_yy_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
I_yy = token_value;
|
|
|
|
|
massParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case I_zz_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
I_zz = token_value;
|
|
|
|
|
massParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case I_xz_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
I_xz = token_value;
|
|
|
|
|
massParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end mass map
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
case engine_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(engine_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case simpleSingle_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
simpleSingleMaxThrust = token_value;
|
|
|
|
|
engineParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case c172_flag:
|
|
|
|
|
{
|
|
|
|
|
engineParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case cherokee_flag:
|
|
|
|
|
{
|
|
|
|
|
engineParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2001-09-14 20:36:34 +00:00
|
|
|
case Throttle_pct_input_flag:
|
|
|
|
|
{
|
|
|
|
|
Throttle_pct_input = true;
|
2002-04-01 21:37:33 +00:00
|
|
|
Throttle_pct_input_file = aircraft_directory + linetoken3;
|
2001-09-14 20:36:34 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
uiuc_1DdataFileReader(Throttle_pct_input_file,
|
|
|
|
|
Throttle_pct_input_timeArray,
|
|
|
|
|
Throttle_pct_input_dTArray,
|
|
|
|
|
Throttle_pct_input_ntime);
|
|
|
|
|
token6 >> token_value;
|
|
|
|
|
Throttle_pct_input_startTime = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end engine map
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
case CD_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(CD_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case CDo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CDo = token_value;
|
|
|
|
|
CDo_clean = CDo;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CDK_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CDK = token_value;
|
|
|
|
|
CDK_clean = CDK;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CD_a = token_value;
|
|
|
|
|
CD_a_clean = CD_a;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_adot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CD_adot = token_value;
|
|
|
|
|
CD_adot_clean = CD_adot;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CD_q = token_value;
|
|
|
|
|
CD_q_clean = CD_q;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_ih_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CD_ih = token_value;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CD_de = token_value;
|
|
|
|
|
CD_de_clean = CD_de;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CDfa_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CDfa = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 1D File Reader with file name (CDfa) and conversion
|
|
|
|
|
factors; function returns array of alphas (aArray) and
|
|
|
|
|
corresponding CD values (CDArray) and max number of
|
|
|
|
|
terms in arrays (nAlpha) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_1DdataFileReader(CDfa,
|
|
|
|
|
CDfa_aArray,
|
|
|
|
|
CDfa_CDArray,
|
|
|
|
|
CDfa_nAlpha);
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CDfCL_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CDfCL = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
/* call 1D File Reader with file name (CDfCL) and conversion
|
|
|
|
|
factors; function returns array of CLs (CLArray) and
|
|
|
|
|
corresponding CD values (CDArray) and max number of
|
|
|
|
|
terms in arrays (nCL) */
|
|
|
|
|
uiuc_1DdataFileReader(CDfCL,
|
|
|
|
|
CDfCL_CLArray,
|
|
|
|
|
CDfCL_CDArray,
|
|
|
|
|
CDfCL_nCL);
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CDfade_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CDfade = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 2D File Reader with file name (CDfade) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CD (CDArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (nde) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_2DdataFileReader(CDfade,
|
|
|
|
|
CDfade_aArray,
|
|
|
|
|
CDfade_deArray,
|
|
|
|
|
CDfade_CDArray,
|
|
|
|
|
CDfade_nAlphaArray,
|
|
|
|
|
CDfade_nde);
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CDfdf_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CDfdf = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
/* call 1D File Reader with file name (CDfdf) and conversion
|
|
|
|
|
factors; function returns array of dfs (dfArray) and
|
|
|
|
|
corresponding CD values (CDArray) and max number of
|
|
|
|
|
terms in arrays (ndf) */
|
|
|
|
|
uiuc_1DdataFileReader(CDfdf,
|
|
|
|
|
CDfdf_dfArray,
|
|
|
|
|
CDfdf_CDArray,
|
|
|
|
|
CDfdf_ndf);
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CDfadf_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CDfadf = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CDfadf) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
flap deflections (dfArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CD (CDArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (ndf) */
|
|
|
|
|
uiuc_2DdataFileReader(CDfadf,
|
|
|
|
|
CDfadf_aArray,
|
|
|
|
|
CDfadf_dfArray,
|
|
|
|
|
CDfadf_CDArray,
|
|
|
|
|
CDfadf_nAlphaArray,
|
|
|
|
|
CDfadf_ndf);
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CXo_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CXo = token_value;
|
|
|
|
|
CXo_clean = CXo;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CXK_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CXK = token_value;
|
|
|
|
|
CXK_clean = CXK;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_a = token_value;
|
|
|
|
|
CX_a_clean = CX_a;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_a2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_a2 = token_value;
|
|
|
|
|
CX_a2_clean = CX_a2;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_a3_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_a3 = token_value;
|
|
|
|
|
CX_a3_clean = CX_a3;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_adot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_adot = token_value;
|
|
|
|
|
CX_adot_clean = CX_adot;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_q = token_value;
|
|
|
|
|
CX_q_clean = CX_q;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_de = token_value;
|
|
|
|
|
CX_de_clean = CX_de;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_dr = token_value;
|
|
|
|
|
CX_dr_clean = CX_dr;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_df_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_df = token_value;
|
|
|
|
|
CX_df_clean = CX_df;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_adf_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CX_adf = token_value;
|
|
|
|
|
CX_adf_clean = CX_adf;
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case CXfabetaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CXfabetaf_index, i;
|
|
|
|
|
string CXfabetaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CXfabetaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CXfabetaf_index;
|
|
|
|
|
if (CXfabetaf_index < 1 || CXfabetaf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CXfabetaf_index > CXfabetaf_nf)
|
|
|
|
|
CXfabetaf_nf = CXfabetaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CXfabetaf_fArray[CXfabetaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CXfabetaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CXfabetaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CXfabetaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CXfabetaf_aArray[CXfabetaf_index] = datafile_xArray;
|
|
|
|
|
CXfabetaf_betaArray[CXfabetaf_index] = datafile_yArray;
|
|
|
|
|
CXfabetaf_CXArray[CXfabetaf_index] = datafile_zArray;
|
|
|
|
|
CXfabetaf_nAlphaArray[CXfabetaf_index] = datafile_nxArray;
|
|
|
|
|
CXfabetaf_nbeta[CXfabetaf_index] = datafile_ny;
|
|
|
|
|
if (CXfabetaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CXfabetaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CXfabetaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CXfabetaf_nb_nice = datafile_ny;
|
|
|
|
|
CXfabetaf_bArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CXfabetaf_na_nice; i++)
|
|
|
|
|
CXfabetaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
CXfabetaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CXfadef_flag:
|
|
|
|
|
{
|
|
|
|
|
int CXfadef_index, i;
|
|
|
|
|
string CXfadef_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CXfadef_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CXfadef_index;
|
|
|
|
|
if (CXfadef_index < 0 || CXfadef_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CXfadef_index > CXfadef_nf)
|
|
|
|
|
CXfadef_nf = CXfadef_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CXfadef_fArray[CXfadef_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CXfadef_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CXfadef_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CXfadef_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CXfadef_aArray[CXfadef_index] = datafile_xArray;
|
|
|
|
|
CXfadef_deArray[CXfadef_index] = datafile_yArray;
|
|
|
|
|
CXfadef_CXArray[CXfadef_index] = datafile_zArray;
|
|
|
|
|
CXfadef_nAlphaArray[CXfadef_index] = datafile_nxArray;
|
|
|
|
|
CXfadef_nde[CXfadef_index] = datafile_ny;
|
|
|
|
|
if (CXfadef_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CXfadef_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CXfadef_na_nice = datafile_nxArray[1];
|
|
|
|
|
CXfadef_nde_nice = datafile_ny;
|
|
|
|
|
CXfadef_deArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CXfadef_na_nice; i++)
|
|
|
|
|
CXfadef_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
CXfadef_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CXfaqf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CXfaqf_index, i;
|
|
|
|
|
string CXfaqf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CXfaqf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CXfaqf_index;
|
|
|
|
|
if (CXfaqf_index < 0 || CXfaqf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CXfaqf_index > CXfaqf_nf)
|
|
|
|
|
CXfaqf_nf = CXfaqf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CXfaqf_fArray[CXfaqf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CXfaqf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CXfaqf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CXfaqf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CXfaqf_aArray[CXfaqf_index] = datafile_xArray;
|
|
|
|
|
CXfaqf_qArray[CXfaqf_index] = datafile_yArray;
|
|
|
|
|
CXfaqf_CXArray[CXfaqf_index] = datafile_zArray;
|
|
|
|
|
CXfaqf_nAlphaArray[CXfaqf_index] = datafile_nxArray;
|
|
|
|
|
CXfaqf_nq[CXfaqf_index] = datafile_ny;
|
|
|
|
|
if (CXfaqf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CXfaqf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CXfaqf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CXfaqf_nq_nice = datafile_ny;
|
|
|
|
|
CXfaqf_qArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CXfaqf_na_nice; i++)
|
|
|
|
|
CXfaqf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroDragParts -> storeCommands (*command_line);
|
|
|
|
|
CXfaqf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end CD map
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
case CL_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(CL_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case CLo_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CLo = token_value;
|
|
|
|
|
CLo_clean = CLo;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CL_a = token_value;
|
|
|
|
|
CL_a_clean = CL_a;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_adot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CL_adot = token_value;
|
|
|
|
|
CL_adot_clean = CL_adot;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CL_q = token_value;
|
|
|
|
|
CL_q_clean = CL_q;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_ih_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CL_ih = token_value;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CL_de = token_value;
|
|
|
|
|
CL_de_clean = CL_de;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CLfa_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CLfa = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 1D File Reader with file name (CLfa) and conversion
|
|
|
|
|
factors; function returns array of alphas (aArray) and
|
|
|
|
|
corresponding CL values (CLArray) and max number of
|
|
|
|
|
terms in arrays (nAlpha) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_1DdataFileReader(CLfa,
|
|
|
|
|
CLfa_aArray,
|
|
|
|
|
CLfa_CLArray,
|
|
|
|
|
CLfa_nAlpha);
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
2000-03-22 22:01:33 +00:00
|
|
|
}
|
|
|
|
|
case CLfade_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CLfade = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 2D File Reader with file name (CLfade) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CL (CLArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (nde) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_2DdataFileReader(CLfade,
|
|
|
|
|
CLfade_aArray,
|
|
|
|
|
CLfade_deArray,
|
|
|
|
|
CLfade_CLArray,
|
|
|
|
|
CLfade_nAlphaArray,
|
|
|
|
|
CLfade_nde);
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CLfdf_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CLfdf = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
/* call 1D File Reader with file name (CLfdf) and conversion
|
|
|
|
|
factors; function returns array of dfs (dfArray) and
|
|
|
|
|
corresponding CL values (CLArray) and max number of
|
|
|
|
|
terms in arrays (ndf) */
|
|
|
|
|
uiuc_1DdataFileReader(CLfdf,
|
|
|
|
|
CLfdf_dfArray,
|
|
|
|
|
CLfdf_CLArray,
|
|
|
|
|
CLfdf_ndf);
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
|
|
|
|
|
// additional variables to streamline flap routine in aerodeflections
|
|
|
|
|
ndf = CLfdf_ndf;
|
|
|
|
|
int temp_counter = 1;
|
|
|
|
|
while (temp_counter <= ndf)
|
|
|
|
|
{
|
|
|
|
|
dfArray[temp_counter] = CLfdf_dfArray[temp_counter];
|
|
|
|
|
TimeArray[temp_counter] = dfTimefdf_TimeArray[temp_counter];
|
|
|
|
|
temp_counter++;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CLfadf_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CLfadf = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CLfadf) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
flap deflections (dfArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CL (CLArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (ndf) */
|
|
|
|
|
uiuc_2DdataFileReader(CLfadf,
|
|
|
|
|
CLfadf_aArray,
|
|
|
|
|
CLfadf_dfArray,
|
|
|
|
|
CLfadf_CLArray,
|
|
|
|
|
CLfadf_nAlphaArray,
|
|
|
|
|
CLfadf_ndf);
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZo = token_value;
|
|
|
|
|
CZo_clean = CZo;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_a = token_value;
|
|
|
|
|
CZ_a_clean = CZ_a;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_a2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_a2 = token_value;
|
|
|
|
|
CZ_a2_clean = CZ_a2;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_a3_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_a3 = token_value;
|
|
|
|
|
CZ_a3_clean = CZ_a3;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_adot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_adot = token_value;
|
|
|
|
|
CZ_adot_clean = CZ_adot;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_q = token_value;
|
|
|
|
|
CZ_q_clean = CZ_q;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_de = token_value;
|
|
|
|
|
CZ_de_clean = CZ_de;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_deb2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_deb2 = token_value;
|
|
|
|
|
CZ_deb2_clean = CZ_deb2;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_df_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_df = token_value;
|
|
|
|
|
CZ_df_clean = CZ_df;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_adf_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CZ_adf = token_value;
|
|
|
|
|
CZ_adf_clean = CZ_adf;
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2001-09-14 20:36:34 +00:00
|
|
|
case CZfa_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CZfa = aircraft_directory + linetoken3;
|
2001-09-14 20:36:34 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
/* call 1D File Reader with file name (CZfa) and conversion
|
|
|
|
|
factors; function returns array of alphas (aArray) and
|
|
|
|
|
corresponding CZ values (CZArray) and max number of
|
|
|
|
|
terms in arrays (nAlpha) */
|
|
|
|
|
uiuc_1DdataFileReader(CZfa,
|
|
|
|
|
CZfa_aArray,
|
|
|
|
|
CZfa_CZArray,
|
|
|
|
|
CZfa_nAlpha);
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case CZfabetaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CZfabetaf_index, i;
|
|
|
|
|
string CZfabetaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CZfabetaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CZfabetaf_index;
|
|
|
|
|
if (CZfabetaf_index < 0 || CZfabetaf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CZfabetaf_index > CZfabetaf_nf)
|
|
|
|
|
CZfabetaf_nf = CZfabetaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CZfabetaf_fArray[CZfabetaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CZfabetaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CZfabetaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
beta (betaArray) and corresponding
|
|
|
|
|
alpha (aArray) and CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and beta array (nbeta) */
|
|
|
|
|
uiuc_2DdataFileReader(CZfabetaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CZfabetaf_aArray[CZfabetaf_index] = datafile_xArray;
|
|
|
|
|
CZfabetaf_betaArray[CZfabetaf_index] = datafile_yArray;
|
|
|
|
|
CZfabetaf_CZArray[CZfabetaf_index] = datafile_zArray;
|
|
|
|
|
CZfabetaf_nAlphaArray[CZfabetaf_index] = datafile_nxArray;
|
|
|
|
|
CZfabetaf_nbeta[CZfabetaf_index] = datafile_ny;
|
|
|
|
|
if (CZfabetaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CZfabetaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CZfabetaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CZfabetaf_nb_nice = datafile_ny;
|
|
|
|
|
CZfabetaf_bArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CZfabetaf_na_nice; i++)
|
|
|
|
|
CZfabetaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
CZfabetaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZfadef_flag:
|
|
|
|
|
{
|
|
|
|
|
int CZfadef_index, i;
|
|
|
|
|
string CZfadef_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CZfadef_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CZfadef_index;
|
|
|
|
|
if (CZfadef_index < 0 || CZfadef_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CZfadef_index > CZfadef_nf)
|
|
|
|
|
CZfadef_nf = CZfadef_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CZfadef_fArray[CZfadef_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CZfadef_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CZfadef_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CZfadef_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CZfadef_aArray[CZfadef_index] = datafile_xArray;
|
|
|
|
|
CZfadef_deArray[CZfadef_index] = datafile_yArray;
|
|
|
|
|
CZfadef_CZArray[CZfadef_index] = datafile_zArray;
|
|
|
|
|
CZfadef_nAlphaArray[CZfadef_index] = datafile_nxArray;
|
|
|
|
|
CZfadef_nde[CZfadef_index] = datafile_ny;
|
|
|
|
|
if (CZfadef_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CZfadef_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CZfadef_na_nice = datafile_nxArray[1];
|
|
|
|
|
CZfadef_nde_nice = datafile_ny;
|
|
|
|
|
CZfadef_deArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CZfadef_na_nice; i++)
|
|
|
|
|
CZfadef_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
CZfadef_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZfaqf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CZfaqf_index, i;
|
|
|
|
|
string CZfaqf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CZfaqf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CZfaqf_index;
|
|
|
|
|
if (CZfaqf_index < 0 || CZfaqf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CZfaqf_index > CZfaqf_nf)
|
|
|
|
|
CZfaqf_nf = CZfaqf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CZfaqf_fArray[CZfaqf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CZfaqf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CZfaqf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
pitch rate (qArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and pitch rate array (nq) */
|
|
|
|
|
uiuc_2DdataFileReader(CZfaqf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CZfaqf_aArray[CZfaqf_index] = datafile_xArray;
|
|
|
|
|
CZfaqf_qArray[CZfaqf_index] = datafile_yArray;
|
|
|
|
|
CZfaqf_CZArray[CZfaqf_index] = datafile_zArray;
|
|
|
|
|
CZfaqf_nAlphaArray[CZfaqf_index] = datafile_nxArray;
|
|
|
|
|
CZfaqf_nq[CZfaqf_index] = datafile_ny;
|
|
|
|
|
if (CZfaqf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CZfaqf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CZfaqf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CZfaqf_nq_nice = datafile_ny;
|
|
|
|
|
CZfaqf_qArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CZfaqf_na_nice; i++)
|
|
|
|
|
CZfaqf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroLiftParts -> storeCommands (*command_line);
|
|
|
|
|
CZfaqf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
2000-09-06 19:52:37 +00:00
|
|
|
break;
|
2000-03-22 22:01:33 +00:00
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end CL map
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
case Cm_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(Cm_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case Cmo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cmo = token_value;
|
|
|
|
|
Cmo_clean = Cmo;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_a = token_value;
|
|
|
|
|
Cm_a_clean = Cm_a;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_a2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_a2 = token_value;
|
|
|
|
|
Cm_a2_clean = Cm_a2;
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_adot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_adot = token_value;
|
|
|
|
|
Cm_adot_clean = Cm_adot;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_q = token_value;
|
|
|
|
|
Cm_q_clean = Cm_q;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_ih_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_ih = token_value;
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_de = token_value;
|
|
|
|
|
Cm_de_clean = Cm_de;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_b2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_b2 = token_value;
|
|
|
|
|
Cm_b2_clean = Cm_b2;
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_r_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_r = token_value;
|
|
|
|
|
Cm_r_clean = Cm_r;
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_df_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cm_df = token_value;
|
|
|
|
|
Cm_df_clean = Cm_df;
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cmfa_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
Cmfa = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
/* call 1D File Reader with file name (Cmfa) and conversion
|
|
|
|
|
factors; function returns array of alphas (aArray) and
|
|
|
|
|
corresponding Cm values (CmArray) and max number of
|
|
|
|
|
terms in arrays (nAlpha) */
|
|
|
|
|
uiuc_1DdataFileReader(Cmfa,
|
|
|
|
|
Cmfa_aArray,
|
|
|
|
|
Cmfa_CmArray,
|
|
|
|
|
Cmfa_nAlpha);
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cmfade_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
Cmfade = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 2D File Reader with file name (Cmfade) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta Cm (CmArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (nde) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_2DdataFileReader(Cmfade,
|
|
|
|
|
Cmfade_aArray,
|
|
|
|
|
Cmfade_deArray,
|
|
|
|
|
Cmfade_CmArray,
|
|
|
|
|
Cmfade_nAlphaArray,
|
|
|
|
|
Cmfade_nde);
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cmfdf_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
Cmfdf = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
/* call 1D File Reader with file name (Cmfdf) and conversion
|
|
|
|
|
factors; function returns array of dfs (dfArray) and
|
|
|
|
|
corresponding Cm values (CmArray) and max number of
|
|
|
|
|
terms in arrays (ndf) */
|
|
|
|
|
uiuc_1DdataFileReader(Cmfdf,
|
|
|
|
|
Cmfdf_dfArray,
|
|
|
|
|
Cmfdf_CmArray,
|
|
|
|
|
Cmfdf_ndf);
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cmfadf_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
Cmfadf = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cmfadf) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
flap deflections (dfArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta Cm (CmArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (ndf) */
|
|
|
|
|
uiuc_2DdataFileReader(Cmfadf,
|
|
|
|
|
Cmfadf_aArray,
|
|
|
|
|
Cmfadf_dfArray,
|
|
|
|
|
Cmfadf_CmArray,
|
|
|
|
|
Cmfadf_nAlphaArray,
|
|
|
|
|
Cmfadf_ndf);
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case Cmfabetaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Cmfabetaf_index, i;
|
|
|
|
|
string Cmfabetaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Cmfabetaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Cmfabetaf_index;
|
|
|
|
|
if (Cmfabetaf_index < 0 || Cmfabetaf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Cmfabetaf_index > Cmfabetaf_nf)
|
|
|
|
|
Cmfabetaf_nf = Cmfabetaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Cmfabetaf_fArray[Cmfabetaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Cmfabetaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cmfabetaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Cmfabetaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Cmfabetaf_aArray[Cmfabetaf_index] = datafile_xArray;
|
|
|
|
|
Cmfabetaf_betaArray[Cmfabetaf_index] = datafile_yArray;
|
|
|
|
|
Cmfabetaf_CmArray[Cmfabetaf_index] = datafile_zArray;
|
|
|
|
|
Cmfabetaf_nAlphaArray[Cmfabetaf_index] = datafile_nxArray;
|
|
|
|
|
Cmfabetaf_nbeta[Cmfabetaf_index] = datafile_ny;
|
|
|
|
|
if (Cmfabetaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Cmfabetaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Cmfabetaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Cmfabetaf_nb_nice = datafile_ny;
|
|
|
|
|
Cmfabetaf_bArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Cmfabetaf_na_nice; i++)
|
|
|
|
|
Cmfabetaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
Cmfabetaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cmfadef_flag:
|
|
|
|
|
{
|
|
|
|
|
int Cmfadef_index, i;
|
|
|
|
|
string Cmfadef_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Cmfadef_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Cmfadef_index;
|
|
|
|
|
if (Cmfadef_index < 0 || Cmfadef_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Cmfadef_index > Cmfadef_nf)
|
|
|
|
|
Cmfadef_nf = Cmfadef_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Cmfadef_fArray[Cmfadef_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Cmfadef_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cmfadef_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Cmfadef_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Cmfadef_aArray[Cmfadef_index] = datafile_xArray;
|
|
|
|
|
Cmfadef_deArray[Cmfadef_index] = datafile_yArray;
|
|
|
|
|
Cmfadef_CmArray[Cmfadef_index] = datafile_zArray;
|
|
|
|
|
Cmfadef_nAlphaArray[Cmfadef_index] = datafile_nxArray;
|
|
|
|
|
Cmfadef_nde[Cmfadef_index] = datafile_ny;
|
|
|
|
|
if (Cmfadef_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Cmfadef_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Cmfadef_na_nice = datafile_nxArray[1];
|
|
|
|
|
Cmfadef_nde_nice = datafile_ny;
|
|
|
|
|
Cmfadef_deArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Cmfadef_na_nice; i++)
|
|
|
|
|
Cmfadef_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
Cmfadef_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cmfaqf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Cmfaqf_index, i;
|
|
|
|
|
string Cmfaqf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Cmfaqf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Cmfaqf_index;
|
|
|
|
|
if (Cmfaqf_index < 0 || Cmfaqf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Cmfaqf_index > Cmfaqf_nf)
|
|
|
|
|
Cmfaqf_nf = Cmfaqf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Cmfaqf_fArray[Cmfaqf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Cmfaqf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cmfaqf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Cmfaqf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Cmfaqf_aArray[Cmfaqf_index] = datafile_xArray;
|
|
|
|
|
Cmfaqf_qArray[Cmfaqf_index] = datafile_yArray;
|
|
|
|
|
Cmfaqf_CmArray[Cmfaqf_index] = datafile_zArray;
|
|
|
|
|
Cmfaqf_nAlphaArray[Cmfaqf_index] = datafile_nxArray;
|
|
|
|
|
Cmfaqf_nq[Cmfaqf_index] = datafile_ny;
|
|
|
|
|
if (Cmfaqf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Cmfaqf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Cmfaqf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Cmfaqf_nq_nice = datafile_ny;
|
|
|
|
|
Cmfaqf_qArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Cmfaqf_na_nice; i++)
|
|
|
|
|
Cmfaqf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroPitchParts -> storeCommands (*command_line);
|
|
|
|
|
Cmfaqf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end Cm map
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
case CY_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(CY_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case CYo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CYo = token_value;
|
|
|
|
|
CYo_clean = CYo;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_beta_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CY_beta = token_value;
|
|
|
|
|
CY_beta_clean = CY_beta;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_p_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CY_p = token_value;
|
|
|
|
|
CY_p_clean = CY_p;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_r_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CY_r = token_value;
|
|
|
|
|
CY_r_clean = CY_r;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_da_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
CY_da = token_value;
|
|
|
|
|
CY_da_clean = CY_da;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
|
|
|
|
|
CY_dr = token_value;
|
|
|
|
|
CY_dr_clean = CY_dr;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CY_dra_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
|
|
|
|
|
CY_dra = token_value;
|
|
|
|
|
CY_dra_clean = CY_dra;
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_bdot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
|
|
|
|
|
CY_bdot = token_value;
|
|
|
|
|
CY_bdot_clean = CY_bdot;
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfada_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CYfada = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CYfada) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
aileron deflections (daArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CY (CYArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (nda) */
|
|
|
|
|
uiuc_2DdataFileReader(CYfada,
|
|
|
|
|
CYfada_aArray,
|
|
|
|
|
CYfada_daArray,
|
|
|
|
|
CYfada_CYArray,
|
|
|
|
|
CYfada_nAlphaArray,
|
|
|
|
|
CYfada_nda);
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfbetadr_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
CYfbetadr = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 2D File Reader with file name (CYfbetadr) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
rudder deflections (drArray) and corresponding
|
|
|
|
|
beta (betaArray) and delta CY (CYArray) values and
|
|
|
|
|
max number of terms in beta arrays (nBetaArray)
|
|
|
|
|
and deflection array (ndr) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_2DdataFileReader(CYfbetadr,
|
|
|
|
|
CYfbetadr_betaArray,
|
|
|
|
|
CYfbetadr_drArray,
|
|
|
|
|
CYfbetadr_CYArray,
|
|
|
|
|
CYfbetadr_nBetaArray,
|
|
|
|
|
CYfbetadr_ndr);
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case CYfabetaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CYfabetaf_index, i;
|
|
|
|
|
string CYfabetaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CYfabetaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CYfabetaf_index;
|
|
|
|
|
if (CYfabetaf_index < 0 || CYfabetaf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CYfabetaf_index > CYfabetaf_nf)
|
|
|
|
|
CYfabetaf_nf = CYfabetaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CYfabetaf_fArray[CYfabetaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CYfabetaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CYfabetaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CYfabetaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CYfabetaf_aArray[CYfabetaf_index] = datafile_xArray;
|
|
|
|
|
CYfabetaf_betaArray[CYfabetaf_index] = datafile_yArray;
|
|
|
|
|
CYfabetaf_CYArray[CYfabetaf_index] = datafile_zArray;
|
|
|
|
|
CYfabetaf_nAlphaArray[CYfabetaf_index] = datafile_nxArray;
|
|
|
|
|
CYfabetaf_nbeta[CYfabetaf_index] = datafile_ny;
|
|
|
|
|
if (CYfabetaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CYfabetaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CYfabetaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CYfabetaf_nb_nice = datafile_ny;
|
|
|
|
|
CYfabetaf_bArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CYfabetaf_na_nice; i++)
|
|
|
|
|
CYfabetaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
|
|
|
|
CYfabetaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfadaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CYfadaf_index, i;
|
|
|
|
|
string CYfadaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CYfadaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CYfadaf_index;
|
|
|
|
|
if (CYfadaf_index < 0 || CYfadaf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CYfadaf_index > CYfadaf_nf)
|
|
|
|
|
CYfadaf_nf = CYfadaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CYfadaf_fArray[CYfadaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CYfadaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CYfadaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CYfadaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CYfadaf_aArray[CYfadaf_index] = datafile_xArray;
|
|
|
|
|
CYfadaf_daArray[CYfadaf_index] = datafile_yArray;
|
|
|
|
|
CYfadaf_CYArray[CYfadaf_index] = datafile_zArray;
|
|
|
|
|
CYfadaf_nAlphaArray[CYfadaf_index] = datafile_nxArray;
|
|
|
|
|
CYfadaf_nda[CYfadaf_index] = datafile_ny;
|
|
|
|
|
if (CYfadaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CYfadaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CYfadaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CYfadaf_nda_nice = datafile_ny;
|
|
|
|
|
CYfadaf_daArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CYfadaf_na_nice; i++)
|
|
|
|
|
CYfadaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
|
|
|
|
CYfadaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfadrf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CYfadrf_index, i;
|
|
|
|
|
string CYfadrf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CYfadrf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CYfadrf_index;
|
|
|
|
|
if (CYfadrf_index < 0 || CYfadrf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CYfadrf_index > CYfadrf_nf)
|
|
|
|
|
CYfadrf_nf = CYfadrf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CYfadrf_fArray[CYfadrf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CYfadrf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CYfadrf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CYfadrf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CYfadrf_aArray[CYfadrf_index] = datafile_xArray;
|
|
|
|
|
CYfadrf_drArray[CYfadrf_index] = datafile_yArray;
|
|
|
|
|
CYfadrf_CYArray[CYfadrf_index] = datafile_zArray;
|
|
|
|
|
CYfadrf_nAlphaArray[CYfadrf_index] = datafile_nxArray;
|
|
|
|
|
CYfadrf_ndr[CYfadrf_index] = datafile_ny;
|
|
|
|
|
if (CYfadrf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CYfadrf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CYfadrf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CYfadrf_ndr_nice = datafile_ny;
|
|
|
|
|
CYfadrf_drArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CYfadrf_na_nice; i++)
|
|
|
|
|
CYfadrf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
|
|
|
|
CYfadrf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfapf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CYfapf_index, i;
|
|
|
|
|
string CYfapf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CYfapf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CYfapf_index;
|
|
|
|
|
if (CYfapf_index < 0 || CYfapf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CYfapf_index > CYfapf_nf)
|
|
|
|
|
CYfapf_nf = CYfapf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CYfapf_fArray[CYfapf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CYfapf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CYfapf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CYfapf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CYfapf_aArray[CYfapf_index] = datafile_xArray;
|
|
|
|
|
CYfapf_pArray[CYfapf_index] = datafile_yArray;
|
|
|
|
|
CYfapf_CYArray[CYfapf_index] = datafile_zArray;
|
|
|
|
|
CYfapf_nAlphaArray[CYfapf_index] = datafile_nxArray;
|
|
|
|
|
CYfapf_np[CYfapf_index] = datafile_ny;
|
|
|
|
|
if (CYfapf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CYfapf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CYfapf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CYfapf_np_nice = datafile_ny;
|
|
|
|
|
CYfapf_pArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CYfapf_na_nice; i++)
|
|
|
|
|
CYfapf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
|
|
|
|
CYfapf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfarf_flag:
|
|
|
|
|
{
|
|
|
|
|
int CYfarf_index, i;
|
|
|
|
|
string CYfarf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
CYfarf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> CYfarf_index;
|
|
|
|
|
if (CYfarf_index < 0 || CYfarf_index >= 30)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (CYfarf_index > CYfarf_nf)
|
|
|
|
|
CYfarf_nf = CYfarf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
CYfarf_fArray[CYfarf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> CYfarf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (CYfarf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(CYfarf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
CYfarf_aArray[CYfarf_index] = datafile_xArray;
|
|
|
|
|
CYfarf_rArray[CYfarf_index] = datafile_yArray;
|
|
|
|
|
CYfarf_CYArray[CYfarf_index] = datafile_zArray;
|
|
|
|
|
CYfarf_nAlphaArray[CYfarf_index] = datafile_nxArray;
|
|
|
|
|
CYfarf_nr[CYfarf_index] = datafile_ny;
|
|
|
|
|
if (CYfarf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (CYfarf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
CYfarf_na_nice = datafile_nxArray[1];
|
|
|
|
|
CYfarf_nr_nice = datafile_ny;
|
|
|
|
|
CYfarf_rArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=CYfarf_na_nice; i++)
|
|
|
|
|
CYfarf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroSideforceParts -> storeCommands (*command_line);
|
|
|
|
|
CYfarf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
2000-09-06 19:52:37 +00:00
|
|
|
break;
|
2000-03-22 22:01:33 +00:00
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end CY map
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
case Cl_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(Cl_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case Clo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Clo = token_value;
|
|
|
|
|
Clo_clean = Clo;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_beta_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cl_beta = token_value;
|
|
|
|
|
Cl_beta_clean = Cl_beta;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_p_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cl_p = token_value;
|
|
|
|
|
Cl_p_clean = Cl_p;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_r_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cl_r = token_value;
|
|
|
|
|
Cl_r_clean = Cl_r;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_da_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cl_da = token_value;
|
|
|
|
|
Cl_da_clean = Cl_da;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cl_dr = token_value;
|
|
|
|
|
Cl_dr_clean = Cl_dr;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_daa_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cl_daa = token_value;
|
|
|
|
|
Cl_daa_clean = Cl_daa;
|
|
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Clfada_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
Clfada = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 2D File Reader with file name (Clfada) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
aileron deflections (daArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta Cl (ClArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (nda) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_2DdataFileReader(Clfada,
|
|
|
|
|
Clfada_aArray,
|
|
|
|
|
Clfada_daArray,
|
|
|
|
|
Clfada_ClArray,
|
|
|
|
|
Clfada_nAlphaArray,
|
|
|
|
|
Clfada_nda);
|
|
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Clfbetadr_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
Clfbetadr = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 2D File Reader with file name (Clfbetadr) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
rudder deflections (drArray) and corresponding
|
|
|
|
|
beta (betaArray) and delta Cl (ClArray) values and
|
|
|
|
|
max number of terms in beta arrays (nBetaArray)
|
|
|
|
|
and deflection array (ndr) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_2DdataFileReader(Clfbetadr,
|
|
|
|
|
Clfbetadr_betaArray,
|
|
|
|
|
Clfbetadr_drArray,
|
|
|
|
|
Clfbetadr_ClArray,
|
|
|
|
|
Clfbetadr_nBetaArray,
|
|
|
|
|
Clfbetadr_ndr);
|
|
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case Clfabetaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Clfabetaf_index, i;
|
|
|
|
|
string Clfabetaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Clfabetaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Clfabetaf_index;
|
|
|
|
|
if (Clfabetaf_index < 0 || Clfabetaf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Clfabetaf_index > Clfabetaf_nf)
|
|
|
|
|
Clfabetaf_nf = Clfabetaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Clfabetaf_fArray[Clfabetaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Clfabetaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Clfabetaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Clfabetaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Clfabetaf_aArray[Clfabetaf_index] = datafile_xArray;
|
|
|
|
|
Clfabetaf_betaArray[Clfabetaf_index] = datafile_yArray;
|
|
|
|
|
Clfabetaf_ClArray[Clfabetaf_index] = datafile_zArray;
|
|
|
|
|
Clfabetaf_nAlphaArray[Clfabetaf_index] = datafile_nxArray;
|
|
|
|
|
Clfabetaf_nbeta[Clfabetaf_index] = datafile_ny;
|
|
|
|
|
if (Clfabetaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Clfabetaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Clfabetaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Clfabetaf_nb_nice = datafile_ny;
|
|
|
|
|
Clfabetaf_bArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Clfabetaf_na_nice; i++)
|
|
|
|
|
Clfabetaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
|
|
|
|
Clfabetaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Clfadaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Clfadaf_index, i;
|
|
|
|
|
string Clfadaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Clfadaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Clfadaf_index;
|
|
|
|
|
if (Clfadaf_index < 0 || Clfadaf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Clfadaf_index > Clfadaf_nf)
|
|
|
|
|
Clfadaf_nf = Clfadaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Clfadaf_fArray[Clfadaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Clfadaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Clfadaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Clfadaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Clfadaf_aArray[Clfadaf_index] = datafile_xArray;
|
|
|
|
|
Clfadaf_daArray[Clfadaf_index] = datafile_yArray;
|
|
|
|
|
Clfadaf_ClArray[Clfadaf_index] = datafile_zArray;
|
|
|
|
|
Clfadaf_nAlphaArray[Clfadaf_index] = datafile_nxArray;
|
|
|
|
|
Clfadaf_nda[Clfadaf_index] = datafile_ny;
|
|
|
|
|
if (Clfadaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Clfadaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Clfadaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Clfadaf_nda_nice = datafile_ny;
|
|
|
|
|
Clfadaf_daArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Clfadaf_na_nice; i++)
|
|
|
|
|
Clfadaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
|
|
|
|
Clfadaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Clfadrf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Clfadrf_index, i;
|
|
|
|
|
string Clfadrf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Clfadrf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Clfadrf_index;
|
|
|
|
|
if (Clfadrf_index < 0 || Clfadrf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Clfadrf_index > Clfadrf_nf)
|
|
|
|
|
Clfadrf_nf = Clfadrf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Clfadrf_fArray[Clfadrf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Clfadrf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Clfadrf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Clfadrf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Clfadrf_aArray[Clfadrf_index] = datafile_xArray;
|
|
|
|
|
Clfadrf_drArray[Clfadrf_index] = datafile_yArray;
|
|
|
|
|
Clfadrf_ClArray[Clfadrf_index] = datafile_zArray;
|
|
|
|
|
Clfadrf_nAlphaArray[Clfadrf_index] = datafile_nxArray;
|
|
|
|
|
Clfadrf_ndr[Clfadrf_index] = datafile_ny;
|
|
|
|
|
if (Clfadrf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Clfadrf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Clfadrf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Clfadrf_ndr_nice = datafile_ny;
|
|
|
|
|
Clfadrf_drArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Clfadrf_na_nice; i++)
|
|
|
|
|
Clfadrf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
|
|
|
|
Clfadrf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Clfapf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Clfapf_index, i;
|
|
|
|
|
string Clfapf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Clfapf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Clfapf_index;
|
|
|
|
|
if (Clfapf_index < 0 || Clfapf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Clfapf_index > Clfapf_nf)
|
|
|
|
|
Clfapf_nf = Clfapf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Clfapf_fArray[Clfapf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Clfapf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Clfapf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Clfapf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Clfapf_aArray[Clfapf_index] = datafile_xArray;
|
|
|
|
|
Clfapf_pArray[Clfapf_index] = datafile_yArray;
|
|
|
|
|
Clfapf_ClArray[Clfapf_index] = datafile_zArray;
|
|
|
|
|
Clfapf_nAlphaArray[Clfapf_index] = datafile_nxArray;
|
|
|
|
|
Clfapf_np[Clfapf_index] = datafile_ny;
|
|
|
|
|
if (Clfapf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Clfapf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Clfapf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Clfapf_np_nice = datafile_ny;
|
|
|
|
|
Clfapf_pArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Clfapf_na_nice; i++)
|
|
|
|
|
Clfapf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
|
|
|
|
Clfapf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Clfarf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Clfarf_index, i;
|
|
|
|
|
string Clfarf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Clfarf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Clfarf_index;
|
|
|
|
|
if (Clfarf_index < 0 || Clfarf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Clfarf_index > Clfarf_nf)
|
|
|
|
|
Clfarf_nf = Clfarf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Clfarf_fArray[Clfarf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Clfarf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Clfarf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Clfarf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Clfarf_aArray[Clfarf_index] = datafile_xArray;
|
|
|
|
|
Clfarf_rArray[Clfarf_index] = datafile_yArray;
|
|
|
|
|
Clfarf_ClArray[Clfarf_index] = datafile_zArray;
|
|
|
|
|
Clfarf_nAlphaArray[Clfarf_index] = datafile_nxArray;
|
|
|
|
|
Clfarf_nr[Clfarf_index] = datafile_ny;
|
|
|
|
|
if (Clfarf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Clfarf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Clfarf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Clfarf_nr_nice = datafile_ny;
|
|
|
|
|
Clfarf_rArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Clfarf_na_nice; i++)
|
|
|
|
|
Clfarf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroRollParts -> storeCommands (*command_line);
|
|
|
|
|
Clfarf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
2002-04-01 21:37:33 +00:00
|
|
|
break;
|
2000-03-22 22:01:33 +00:00
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end Cl map
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
case Cn_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(Cn_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case Cno_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cno = token_value;
|
|
|
|
|
Cno_clean = Cno;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_beta_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cn_beta = token_value;
|
|
|
|
|
Cn_beta_clean = Cn_beta;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_p_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cn_p = token_value;
|
|
|
|
|
Cn_p_clean = Cn_p;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_r_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cn_r = token_value;
|
|
|
|
|
Cn_r_clean = Cn_r;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_da_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cn_da = token_value;
|
|
|
|
|
Cn_da_clean = Cn_da;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cn_dr = token_value;
|
|
|
|
|
Cn_dr_clean = Cn_dr;
|
2000-09-06 19:52:37 +00:00
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cn_q = token_value;
|
|
|
|
|
Cn_q_clean = Cn_q;
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_b3_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
Cn_b3 = token_value;
|
|
|
|
|
Cn_b3_clean = Cn_b3;
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cnfada_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
Cnfada = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 2D File Reader with file name (Cnfada) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
aileron deflections (daArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta Cn (CnArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and deflection array (nda) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_2DdataFileReader(Cnfada,
|
|
|
|
|
Cnfada_aArray,
|
|
|
|
|
Cnfada_daArray,
|
|
|
|
|
Cnfada_CnArray,
|
|
|
|
|
Cnfada_nAlphaArray,
|
|
|
|
|
Cnfada_nda);
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cnfbetadr_flag:
|
|
|
|
|
{
|
2002-04-01 21:37:33 +00:00
|
|
|
Cnfbetadr = aircraft_directory + linetoken3;
|
2000-09-06 19:52:37 +00:00
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
token5 >> token_value_convert2;
|
|
|
|
|
token6 >> token_value_convert3;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
2000-03-22 22:01:33 +00:00
|
|
|
/* call 2D File Reader with file name (Cnfbetadr) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
rudder deflections (drArray) and corresponding
|
|
|
|
|
beta (betaArray) and delta Cn (CnArray) values and
|
|
|
|
|
max number of terms in beta arrays (nBetaArray)
|
|
|
|
|
and deflection array (ndr) */
|
2000-09-06 19:52:37 +00:00
|
|
|
uiuc_2DdataFileReader(Cnfbetadr,
|
|
|
|
|
Cnfbetadr_betaArray,
|
|
|
|
|
Cnfbetadr_drArray,
|
|
|
|
|
Cnfbetadr_CnArray,
|
|
|
|
|
Cnfbetadr_nBetaArray,
|
|
|
|
|
Cnfbetadr_ndr);
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case Cnfabetaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Cnfabetaf_index, i;
|
|
|
|
|
string Cnfabetaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Cnfabetaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Cnfabetaf_index;
|
|
|
|
|
if (Cnfabetaf_index < 0 || Cnfabetaf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Cnfabetaf_index > Cnfabetaf_nf)
|
|
|
|
|
Cnfabetaf_nf = Cnfabetaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Cnfabetaf_fArray[Cnfabetaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Cnfabetaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cnfabetaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Cnfabetaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Cnfabetaf_aArray[Cnfabetaf_index] = datafile_xArray;
|
|
|
|
|
Cnfabetaf_betaArray[Cnfabetaf_index] = datafile_yArray;
|
|
|
|
|
Cnfabetaf_CnArray[Cnfabetaf_index] = datafile_zArray;
|
|
|
|
|
Cnfabetaf_nAlphaArray[Cnfabetaf_index] = datafile_nxArray;
|
|
|
|
|
Cnfabetaf_nbeta[Cnfabetaf_index] = datafile_ny;
|
|
|
|
|
if (Cnfabetaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Cnfabetaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Cnfabetaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Cnfabetaf_nb_nice = datafile_ny;
|
|
|
|
|
Cnfabetaf_bArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Cnfabetaf_na_nice; i++)
|
|
|
|
|
Cnfabetaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
|
|
|
|
Cnfabetaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cnfadaf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Cnfadaf_index, i;
|
|
|
|
|
string Cnfadaf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Cnfadaf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Cnfadaf_index;
|
|
|
|
|
if (Cnfadaf_index < 0 || Cnfadaf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Cnfadaf_index > Cnfadaf_nf)
|
|
|
|
|
Cnfadaf_nf = Cnfadaf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Cnfadaf_fArray[Cnfadaf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Cnfadaf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cnfadaf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Cnfadaf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Cnfadaf_aArray[Cnfadaf_index] = datafile_xArray;
|
|
|
|
|
Cnfadaf_daArray[Cnfadaf_index] = datafile_yArray;
|
|
|
|
|
Cnfadaf_CnArray[Cnfadaf_index] = datafile_zArray;
|
|
|
|
|
Cnfadaf_nAlphaArray[Cnfadaf_index] = datafile_nxArray;
|
|
|
|
|
Cnfadaf_nda[Cnfadaf_index] = datafile_ny;
|
|
|
|
|
if (Cnfadaf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Cnfadaf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Cnfadaf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Cnfadaf_nda_nice = datafile_ny;
|
|
|
|
|
Cnfadaf_daArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Cnfadaf_na_nice; i++)
|
|
|
|
|
Cnfadaf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
|
|
|
|
Cnfadaf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cnfadrf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Cnfadrf_index, i;
|
|
|
|
|
string Cnfadrf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Cnfadrf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Cnfadrf_index;
|
|
|
|
|
if (Cnfadrf_index < 0 || Cnfadrf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Cnfadrf_index > Cnfadrf_nf)
|
|
|
|
|
Cnfadrf_nf = Cnfadrf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Cnfadrf_fArray[Cnfadrf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Cnfadrf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cnfadrf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Cnfadrf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Cnfadrf_aArray[Cnfadrf_index] = datafile_xArray;
|
|
|
|
|
Cnfadrf_drArray[Cnfadrf_index] = datafile_yArray;
|
|
|
|
|
Cnfadrf_CnArray[Cnfadrf_index] = datafile_zArray;
|
|
|
|
|
Cnfadrf_nAlphaArray[Cnfadrf_index] = datafile_nxArray;
|
|
|
|
|
Cnfadrf_ndr[Cnfadrf_index] = datafile_ny;
|
|
|
|
|
if (Cnfadrf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Cnfadrf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Cnfadrf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Cnfadrf_ndr_nice = datafile_ny;
|
|
|
|
|
Cnfadrf_drArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Cnfadrf_na_nice; i++)
|
|
|
|
|
Cnfadrf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
|
|
|
|
Cnfadrf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cnfapf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Cnfapf_index, i;
|
|
|
|
|
string Cnfapf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Cnfapf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Cnfapf_index;
|
|
|
|
|
if (Cnfapf_index < 0 || Cnfapf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Cnfapf_index > Cnfapf_nf)
|
|
|
|
|
Cnfapf_nf = Cnfapf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Cnfapf_fArray[Cnfapf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Cnfapf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cnfapf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Cnfapf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Cnfapf_aArray[Cnfapf_index] = datafile_xArray;
|
|
|
|
|
Cnfapf_pArray[Cnfapf_index] = datafile_yArray;
|
|
|
|
|
Cnfapf_CnArray[Cnfapf_index] = datafile_zArray;
|
|
|
|
|
Cnfapf_nAlphaArray[Cnfapf_index] = datafile_nxArray;
|
|
|
|
|
Cnfapf_np[Cnfapf_index] = datafile_ny;
|
|
|
|
|
if (Cnfapf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Cnfapf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Cnfapf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Cnfapf_np_nice = datafile_ny;
|
|
|
|
|
Cnfapf_pArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Cnfapf_na_nice; i++)
|
|
|
|
|
Cnfapf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
|
|
|
|
Cnfapf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cnfarf_flag:
|
|
|
|
|
{
|
|
|
|
|
int Cnfarf_index, i;
|
|
|
|
|
string Cnfarf_file;
|
|
|
|
|
double flap_value;
|
|
|
|
|
Cnfarf_file = aircraft_directory + linetoken3;
|
|
|
|
|
token4 >> Cnfarf_index;
|
|
|
|
|
if (Cnfarf_index < 0 || Cnfarf_index >= 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
if (Cnfarf_index > Cnfarf_nf)
|
|
|
|
|
Cnfarf_nf = Cnfarf_index;
|
|
|
|
|
token5 >> flap_value;
|
|
|
|
|
Cnfarf_fArray[Cnfarf_index] = flap_value;
|
|
|
|
|
token6 >> token_value_convert1;
|
|
|
|
|
token7 >> token_value_convert2;
|
|
|
|
|
token8 >> token_value_convert3;
|
|
|
|
|
token9 >> Cnfarf_nice;
|
|
|
|
|
convert_z = uiuc_convert(token_value_convert1);
|
|
|
|
|
convert_x = uiuc_convert(token_value_convert2);
|
|
|
|
|
convert_y = uiuc_convert(token_value_convert3);
|
|
|
|
|
/* call 2D File Reader with file name (Cnfarf_file) and
|
|
|
|
|
conversion factors; function returns array of
|
|
|
|
|
elevator deflections (deArray) and corresponding
|
|
|
|
|
alpha (aArray) and delta CZ (CZArray) values and
|
|
|
|
|
max number of terms in alpha arrays (nAlphaArray)
|
|
|
|
|
and delfection array (nde) */
|
|
|
|
|
uiuc_2DdataFileReader(Cnfarf_file,
|
|
|
|
|
datafile_xArray,
|
|
|
|
|
datafile_yArray,
|
|
|
|
|
datafile_zArray,
|
|
|
|
|
datafile_nxArray,
|
|
|
|
|
datafile_ny);
|
|
|
|
|
Cnfarf_aArray[Cnfarf_index] = datafile_xArray;
|
|
|
|
|
Cnfarf_rArray[Cnfarf_index] = datafile_yArray;
|
|
|
|
|
Cnfarf_CnArray[Cnfarf_index] = datafile_zArray;
|
|
|
|
|
Cnfarf_nAlphaArray[Cnfarf_index] = datafile_nxArray;
|
|
|
|
|
Cnfarf_nr[Cnfarf_index] = datafile_ny;
|
|
|
|
|
if (Cnfarf_first==true)
|
|
|
|
|
{
|
|
|
|
|
if (Cnfarf_nice == 1)
|
|
|
|
|
{
|
|
|
|
|
Cnfarf_na_nice = datafile_nxArray[1];
|
|
|
|
|
Cnfarf_nr_nice = datafile_ny;
|
|
|
|
|
Cnfarf_rArray_nice = datafile_yArray;
|
|
|
|
|
for (i=1; i<=Cnfarf_na_nice; i++)
|
|
|
|
|
Cnfarf_aArray_nice[i] = datafile_xArray[1][i];
|
|
|
|
|
}
|
|
|
|
|
aeroYawParts -> storeCommands (*command_line);
|
|
|
|
|
Cnfarf_first=false;
|
|
|
|
|
}
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end Cn map
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
case gear_flag:
|
|
|
|
|
{
|
From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
|
|
|
int index;
|
|
|
|
|
token3 >> index;
|
|
|
|
|
if (index < 0 || index >= 16)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
switch(gear_map[linetoken2])
|
|
|
|
|
{
|
From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
|
|
|
case Dx_gear_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
D_gear_v[index][0] = token_value;
|
|
|
|
|
gear_model[index] = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dy_gear_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
D_gear_v[index][1] = token_value;
|
|
|
|
|
gear_model[index] = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dz_gear_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
D_gear_v[index][2] = token_value;
|
|
|
|
|
gear_model[index] = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case cgear_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
cgear[index] = token_value;
|
|
|
|
|
gear_model[index] = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kgear_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
kgear[index] = token_value;
|
|
|
|
|
gear_model[index] = true;
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
|
|
|
case muGear_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
muGear[index] = token_value;
|
|
|
|
|
gear_model[index] = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case strutLength_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token4 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
strutLength[index] = token_value;
|
|
|
|
|
gear_model[index] = true;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
|
|
|
break;
|
2000-03-22 22:01:33 +00:00
|
|
|
}
|
|
|
|
|
};
|
From: David Megginson <david@megginson.com>
I have created a set of patches to provide configurable landing gear
for the UIUC models. The patches (including four new files) are
available at
http://megginson.com/private/fgfs/uiuc-20010309.tar.gz
A modified UIUC configuration file for the Twin Otter (DHC-6) is
available at
http://megginson.com/private/fgfs/aircraft.dat
It should be possible to configure appropriate gear for all of the
UIUC models now. As a bonus, the models also support braking, both
absolute and differential, as well as nose-wheel steering (all of
which are currently missing from the UIUC models) -- when you land,
you don't have to keep rolling off the end of the runway anymore, and
you don't have to bank to steer in a taxi.
My sample configuration file contains absolutely bizarre, wild
guesses, and many places that I didn't even bother to guess properly.
The only actual data I had was the wing-span of the DHC-6 (65ft),
which I used for positioning the wing tips. The wing-tips for this
model actually work now -- I hit the aileron hard while accelerating
for take-off, and the wingtip noticeably strikes the ground and
bounces up (quite dramatic in external view using the DHC-6 model from
Wolfram's site).
Details
-------
The UIUC models now support up to 16 gear points each where a gear
point is anything in the aircraft that can come in contact with the
ground, including the tail and wing-tips. I have added the following
new fields to the UIUC configuration files, where <index> is an
integer between 0 and 15, and <value> is a real number:
gear <index> Dx_gear <value> # x offset from CG [ft]
gear <index> Dy_gear <value> # y offset from CG [ft]
gear <index> Dz_gear <value> # z offset from CG [ft]
gear <index> cgear <value> # spring damping [lbs/ft/sec]
gear <index> kgear <value> # springiness [lbs/ft]
gear <index> muGear <value> # rolling coefficient
gear <index> strutLength <value> # gear travel [ft] (not yet used)
Most of these names were already pencilled into the UIUC documentation
(as TODO items), but I had to make up Dx_gear, Dy_gear, and Dz_gear --
if those are inappropriate, I'd appreciate suggestions for better
names.
It will be necessary to modify the other UIUC configuration files to
include some kind of gear support as well, or the planes will sink
nose-first into the ground down to their CG's (it's actually quite
funny to watch with an external view).
Background
----------
As I frequently remind everyone here, I have no math background worth
spitting at, so I will not even pretend to have done the hard stuff.
The UIUC code uses a copy of a very old version of the LaRCsim
c172_gear.c -- I wanted to update it with Tony Peden's excellent newer
version, which includes differential braking among other goodies (the
UIUC models don't support brakes, period).
I copied the newer code into uiuc_aero.c, and it compiled and ran, but
all of the planes ended up sitting on their tails with their noses in
the air. Since Tony made his gear code nicely parameterized, I
experimented with different values, and found that it wasn't too hard
to balance the Twin Otter by moving the gear back a bit. At first, I
used properties to set different values, but then I decided to
integrate the whole thing properly into the UIUC configuration
framework. Thanks to Tony Peden, who did the real modelling work -- I
can take credit only for two or three hours of integration. It turns
out that Tony's code is generalized enough to deal with a wide range
of different gear structures -- I suspect that it will even work for
the 747, when I get around to trying some values.
2001-03-29 03:16:25 +00:00
|
|
|
break;
|
2000-03-22 22:01:33 +00:00
|
|
|
} // end gear map
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
case ice_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(ice_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case iceTime_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
ice_model = true;
|
2000-03-22 22:01:33 +00:00
|
|
|
iceTime = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case transientTime_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
transientTime = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case eta_ice_final_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
eta_ice_final = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case beta_probe_wing_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
beta_model = true;
|
|
|
|
|
x_probe_wing = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_probe_tail_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
beta_model = true;
|
|
|
|
|
x_probe_tail = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
case kCDo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCDo = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCDK_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCDK = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCD_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCD_a = token_value;
|
2000-09-06 19:52:37 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCD_adot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCD_adot = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCD_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCD_q = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCD_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCD_de = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case kCXo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCXo = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCXK_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCXK = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_a = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_a2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_a2 = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_a3_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_a3 = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_adot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_adot = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_q = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_de = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_dr = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_df_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_df = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCX_adf_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCX_adf = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
case kCLo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCLo = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCL_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCL_a = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCL_adot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCL_adot = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCL_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCL_q = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCL_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCL_de = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case kCZo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCZo = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCZ_a_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCZ_a = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCZ_a2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCZ_a2 = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCZ_a3_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCZ_a3 = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCZ_adot_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
kCZ_adot = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case kCZ_q_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
kCZ_q = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case kCZ_de_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
kCZ_de = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case kCZ_deb2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCZ_deb2 = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCZ_df_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCZ_df = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCZ_adf_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCZ_adf = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCmo_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
kCmo = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case kCm_a_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
kCm_a = token_value;
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case kCm_a2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
kCm_a2 = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCm_adot_flag:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
kCm_adot = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCm_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCm_q = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCm_de_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCm_de = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCm_b2_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCm_b2 = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCm_r_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCm_r = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCm_df_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCm_df = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCYo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCYo = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCY_beta_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCY_beta = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCY_p_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCY_p = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCY_r_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCY_r = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCY_da_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCY_da = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCY_dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCY_dr = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCY_dra_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCY_dra = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCY_bdot_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCY_bdot = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kClo_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kClo = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCl_beta_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCl_beta = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCl_p_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCl_p = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCl_r_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCl_r = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCl_da_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCl_da = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCl_dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCl_dr = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCl_daa_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCl_daa = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCno_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCno = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCn_beta_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCn_beta = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCn_p_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCn_p = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCn_r_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCn_r = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCn_da_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCn_da = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCn_dr_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCn_dr = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCn_q_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCn_q = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case kCn_b3_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
kCn_b3 = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end ice map
|
2001-09-14 20:36:34 +00:00
|
|
|
|
|
|
|
|
|
|
|
|
|
case fog_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(fog_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case fog_segments_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value_convert1;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
if (token_value_convert1 < 1 || token_value_convert1 > 100)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
fog_field = true;
|
|
|
|
|
fog_point_index = 0;
|
|
|
|
|
delete[] fog_time;
|
|
|
|
|
delete[] fog_value;
|
|
|
|
|
fog_segments = token_value_convert1;
|
|
|
|
|
fog_time = new double[fog_segments+1];
|
|
|
|
|
fog_time[0] = 0.0;
|
|
|
|
|
fog_value = new int[fog_segments+1];
|
|
|
|
|
fog_value[0] = 0;
|
|
|
|
|
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case fog_point_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
if (token_value < 0.1)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
if (check_float(linetoken4))
|
|
|
|
|
token4 >> token_value_convert1;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
if (token_value_convert1 < -1000 || token_value_convert1 > 1000)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
if (fog_point_index == fog_segments || fog_point_index == -1)
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
fog_point_index++;
|
|
|
|
|
fog_time[fog_point_index] = token_value;
|
|
|
|
|
fog_value[fog_point_index] = token_value_convert1;
|
|
|
|
|
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end fog map
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
case record_flag:
|
|
|
|
|
{
|
|
|
|
|
static int fout_flag=0;
|
|
|
|
|
if (fout_flag==0)
|
|
|
|
|
{
|
|
|
|
|
fout_flag=-1;
|
|
|
|
|
fout.open("uiuc_record.dat");
|
|
|
|
|
}
|
|
|
|
|
switch(record_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
/************************* Time ************************/
|
|
|
|
|
case Simtime_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case dt_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/************************* Mass ************************/
|
|
|
|
|
case Weight_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Mass_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case I_xx_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case I_yy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case I_zz_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case I_xz_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/*********************** Geometry **********************/
|
|
|
|
|
case Dx_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dy_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dz_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dx_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dy_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dz_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/********************** Positions **********************/
|
|
|
|
|
case Lat_geocentric_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Lon_geocentric_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Radius_to_vehicle_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Latitude_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Longitude_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Altitude_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Phi_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Theta_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Psi_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/******************** Accelerations ********************/
|
|
|
|
|
case V_dot_north_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_dot_east_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_dot_down_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case U_dot_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_dot_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case W_dot_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case A_X_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case A_Y_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case A_Z_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case A_X_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case A_Y_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case A_Z_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case N_X_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case N_Y_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case N_Z_pilot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case N_X_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case N_Y_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case N_Z_cg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case P_dot_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Q_dot_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case R_dot_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/********************** Velocities *********************/
|
|
|
|
|
case V_north_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_east_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_down_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_north_rel_ground_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_east_rel_ground_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_down_rel_ground_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_north_airmass_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_east_airmass_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_down_airmass_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_north_rel_airmass_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_east_rel_airmass_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_down_rel_airmass_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case U_gust_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_gust_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case W_gust_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case U_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case W_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_rel_wind_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_true_kts_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_rel_ground_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_inertial_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_ground_speed_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_equiv_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_equiv_kts_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_calibrated_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_calibrated_kts_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case P_local_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Q_local_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case R_local_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case P_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Q_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case R_body_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case P_total_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Q_total_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case R_total_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Phi_dot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Theta_dot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Psi_dot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Latitude_dot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Longitude_dot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Radius_dot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/************************ Angles ***********************/
|
|
|
|
|
case Alpha_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Alpha_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Alpha_dot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Alpha_dot_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Beta_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Beta_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Beta_dot_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Beta_dot_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Gamma_vert_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Gamma_vert_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Gamma_horiz_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Gamma_horiz_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/**************** Atmospheric Properties ***************/
|
|
|
|
|
case Density_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case V_sound_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Mach_number_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Static_pressure_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Total_pressure_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Impact_pressure_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Dynamic_pressure_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Static_temperature_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Total_temperature_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/******************** Earth Properties *****************/
|
|
|
|
|
case Gravity_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Sea_level_radius_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Earth_position_angle_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Runway_altitude_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Runway_latitude_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Runway_longitude_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Runway_heading_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Radius_to_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case D_pilot_north_of_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case D_pilot_east_of_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case D_pilot_above_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case X_pilot_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Y_pilot_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case H_pilot_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case D_cg_north_of_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case D_cg_east_of_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case D_cg_above_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case X_cg_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Y_cg_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case H_cg_rwy_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/********************* Engine Inputs *******************/
|
|
|
|
|
case Throttle_pct_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Throttle_3_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/******************** Control Inputs *******************/
|
|
|
|
|
case Long_control_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Long_trim_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Long_trim_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case elevator_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case elevator_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Lat_control_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case aileron_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case aileron_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Rudder_pedal_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case rudder_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case rudder_deg_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Flap_handle_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case flap_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case flap_deg_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case flap_goal_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case flap_pos_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-03-22 22:01:33 +00:00
|
|
|
|
2000-09-06 19:52:37 +00:00
|
|
|
/****************** Aero Coefficients ******************/
|
|
|
|
|
case CD_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CDfaI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CDfadeI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CDfdfI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CDfadfI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CX_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case CXfabetafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CXfadefI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CXfaqfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CDo_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CDK_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_a_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_adot_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_q_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_ih_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CD_de_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CXo_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CXK_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_a_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_a2_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_a3_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_adot_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_q_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_de_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_dr_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_df_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CX_adf_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CL_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CLfaI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CLfadeI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CLfdfI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CLfadfI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CZ_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case CZfaI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZfabetafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZfadefI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZfaqfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CLo_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_a_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_adot_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_q_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_ih_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CL_de_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZo_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_a_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_a2_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_a3_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_adot_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_q_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_de_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_deb2_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_df_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CZ_adf_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Cm_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CmfaI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CmfadeI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CmfdfI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
2000-09-06 19:52:37 +00:00
|
|
|
recordParts -> storeCommands (*command_line);
|
2000-03-22 22:01:33 +00:00
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CmfadfI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case CmfabetafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CmfadefI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CmfaqfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cmo_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_a_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_a2_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_adot_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_q_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_ih_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_de_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_b2_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_r_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cm_df_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CY_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CYfadaI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CYfbetadrI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case CYfabetafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfadafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfadrfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfapfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYfarfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CYo_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_beta_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_p_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_r_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_da_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_dr_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_dra_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CY_bdot_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Cl_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case ClfadaI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case ClfbetadrI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case ClfabetafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case ClfadafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case ClfadrfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case ClfapfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case ClfarfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Clo_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_beta_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_p_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_r_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_da_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_dr_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cl_daa_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Cn_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CnfadaI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CnfbetadrI_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2002-04-01 21:37:33 +00:00
|
|
|
case CnfabetafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CnfadafI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CnfadrfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CnfapfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case CnfarfI_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cno_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_beta_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_p_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_r_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_da_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_dr_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_q_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case Cn_b3_save_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
/******************** Ice Detection ********************/
|
|
|
|
|
case CLclean_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CLiced_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CLclean_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case CLiced_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Lift_clean_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Lift_iced_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Lift_clean_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Lift_iced_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Gamma_clean_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Gamma_iced_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Gamma_clean_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Gamma_iced_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case w_clean_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case w_iced_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case w_clean_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case w_iced_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case V_total_clean_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case V_total_iced_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case V_total_clean_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case V_total_iced_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_flow_clean_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_flow_clean_wing_deg_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_flow_iced_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_flow_iced_wing_deg_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_flow_clean_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_flow_clean_tail_deg_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_flow_iced_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case beta_flow_iced_tail_deg_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Dbeta_flow_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Dbeta_flow_wing_deg_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Dbeta_flow_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case Dbeta_flow_tail_deg_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case pct_beta_flow_wing_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case pct_beta_flow_tail_record:
|
2000-03-22 22:01:33 +00:00
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
/************************ Forces ***********************/
|
2000-03-22 22:01:33 +00:00
|
|
|
case F_X_wind_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Y_wind_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Z_wind_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_X_aero_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Y_aero_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Z_aero_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_X_engine_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Y_engine_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Z_engine_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_X_gear_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Y_gear_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Z_gear_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_X_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Y_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_Z_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
2000-09-06 19:52:37 +00:00
|
|
|
case F_north_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_east_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case F_down_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
/*********************** Moments ***********************/
|
2000-03-22 22:01:33 +00:00
|
|
|
case M_l_aero_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_m_aero_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_n_aero_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_l_engine_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_m_engine_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_n_engine_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_l_gear_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_m_gear_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_n_gear_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_l_rp_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_m_rp_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case M_n_rp_record:
|
|
|
|
|
{
|
|
|
|
|
recordParts -> storeCommands (*command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end record map
|
2000-09-06 19:52:37 +00:00
|
|
|
|
|
|
|
|
|
|
|
|
|
case misc_flag:
|
|
|
|
|
{
|
|
|
|
|
switch(misc_map[linetoken2])
|
|
|
|
|
{
|
|
|
|
|
case simpleHingeMomentCoef_flag:
|
|
|
|
|
{
|
|
|
|
|
if (check_float(linetoken3))
|
|
|
|
|
token3 >> token_value;
|
|
|
|
|
else
|
|
|
|
|
uiuc_warnings_errors(1, *command_line);
|
|
|
|
|
|
|
|
|
|
simpleHingeMomentCoef = token_value;
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
case dfTimefdf_flag:
|
|
|
|
|
{
|
|
|
|
|
dfTimefdf = linetoken3;
|
|
|
|
|
/* call 1D File Reader with file name (dfTimefdf);
|
|
|
|
|
function returns array of dfs (dfArray) and
|
|
|
|
|
corresponding time values (TimeArray) and max
|
|
|
|
|
number of terms in arrays (ndf) */
|
|
|
|
|
uiuc_1DdataFileReader(dfTimefdf,
|
|
|
|
|
dfTimefdf_dfArray,
|
|
|
|
|
dfTimefdf_TimeArray,
|
|
|
|
|
dfTimefdf_ndf);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
break;
|
|
|
|
|
} // end misc map
|
|
|
|
|
|
|
|
|
|
|
2000-03-22 22:01:33 +00:00
|
|
|
default:
|
|
|
|
|
{
|
|
|
|
|
if (linetoken1=="*")
|
|
|
|
|
return;
|
|
|
|
|
uiuc_warnings_errors(2, *command_line);
|
|
|
|
|
break;
|
|
|
|
|
}
|
|
|
|
|
};
|
|
|
|
|
} // end keyword map
|
|
|
|
|
|
|
|
|
|
delete airplane;
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
// end menu.cpp
|