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Author SHA1 Message Date
david
195eadc739 Use SG_LOG for debugging messages from the YASim helicopter model. 2003-11-25 18:50:47 +00:00
curt
69f2597a0c Fix an automake squawk. 2003-10-31 21:15:43 +00:00
ehofman
2ca827a3a4 Fix a bug that gets triggered at least in MSVC and gcc-2.95 2003-10-19 09:27:27 +00:00
david
d4b9ca371c Set the RPM from the property tree with each iteration. This allows a
YASim prop model to start with the prop spinning.
2003-10-18 20:07:46 +00:00
david
202e79b4ad Add the ability to set the RPM from the outside. 2003-10-18 20:07:06 +00:00
curt
5161029fc5 Fix a typo which Frederic's compiler flagged. 2003-10-17 19:17:17 +00:00
curt
cca9f49425 Remove and extraneous starting character. 2003-10-17 14:26:23 +00:00
curt
5333f82eb1 Maik Justus: modifications to add helicopter modeling to YASim. 2003-10-16 14:56:13 +00:00
curt
78cad450e6 Initial revision.
Maik Justus: First pass at helicopter support for YASim.
2003-10-16 14:40:13 +00:00
ehofman
f9b85dc2fd Fix a dependency problem 2003-09-25 09:09:35 +00:00
curt
7807a68fa3 Another step towards making aircraft more self contained. YASim aircraft
now read the config file out of the individual aircraft directory rather
than the collective Aircraft-yasim/ directory (which is now obsolete.)
This requires a corresponding update of the base package cvs.
2003-09-20 03:33:06 +00:00
ehofman
3ba01fa762 New automake, new problems. Add $base_LIBS for programs since $LIBS isn't substituted automatically anymore 2003-08-29 09:03:49 +00:00
david
1d4a7659fc Fix drag when engine is shut down, by avoiding negative RPM.
The Propeller class ignored negative RPM but still returned a torque
value, which ratcheted up a higher and higher negative RPM until drag
overwhelmed the aircraft.

In reality, the propeller should windmill at a reasonable postive RPM,
introducing a constant drag on the aircraft -- the propeller should
*not* stop unless the plane is flying very slowly.  That's a future
project.
2003-08-06 21:38:01 +00:00
ehofman
a2b71872ad This fixes the K to F conversion for the EGT output 2003-07-24 14:43:11 +00:00
ehofman
0ff6c68c01 This patch normalizes the heading value YASim reports to the interface 2003-06-28 21:49:45 +00:00
curt
e9f4fc5972 Jim Wilson:
> > Here's a patch to add manual-pitch control to the propeller in YASim.  A new
> > control axis "PROPPITCH" is added.  Requires "manual-pitch" boolean property
> > in the "propeller" tag.
> >
> > Tags and Properties to add in order to enable:
> >
> > manual-pitch="true"
> >
> > <control-input axis="/controls/engines/engine[0]/propeller-pitch"
> > control="PROPPITCH" src0="0" src1="1" dst0="0.40" dst1="0.80"/>
> >
> > Note that for the time being, excessively low RPM or excessively high RPM is
> > brought undercontrol by a scaling range defined in the control-input tag
> > (see "dst0" and "dst1" properties).
2003-05-16 17:27:17 +00:00
curt
3c7bdc31d9 Cosmetic changes for new code moved into simgear to make the naming scheme
better follow simgear conventions.
2003-05-13 03:18:42 +00:00
curt
51c04e9e4c - Added "SG" prefix to sound classes that recently moved to SimGear.
- Cleaned up some minor compiler warnings.
- Moved src/Model/placement.[ch]xx over into simgear/scene/model/
2003-05-09 19:39:48 +00:00
curt
575b3ac98c Working at unraveling and breaking dependencies inside of src/Model.
I split the FGModelPlacement code out into it's own set of source files.
I created two versions of the fgLoad3DModel() routine.  One that is
  unecumbered by a panelnode dependency and one that is.  acmodel.cxx is
  the only place that needs to load an aircraft with instrument panels.
model.[ch]xx are now pretty much free to move over into simgear.
loader.[ch]xx should be able to follow closely behind.
This will be a big step towards being able to move the material management
code over into simgear.
2003-05-08 20:28:46 +00:00
curt
2119db35c3 This is step "1" of probably "many" in the process of separating out the
scene management code and organizing it within simgear.  My strategy is
to identify the code I want to move, and break it's direct flightgear
dependencies.  Then it will be free to move over into the simgear package.

- Moved some property specific code into simgear/props/
- Split out the condition code from fgfs/src/Main/fg_props and put it
  in it's own source file in simgear/props/
- Created a scene subdirectory for scenery, model, and material property
  related code.
- Moved location.[ch]xx into simgear/scene/model/
- The location and condition code had dependencies on flightgear's global
  state (all the globals-> stuff, the flightgear property tree, etc.)  SimGear
  code can't depend on it so that data has to be passed as parameters to the
  functions/methods/constructors.
- This need to pass data as function parameters had a dramatic cascading
  effect throughout the FlightGear code.
2003-05-06 23:46:24 +00:00
david
7ba6807736 Fix to use renamed /controls properties. 2003-04-01 15:51:15 +00:00
ehofman
c3cefaf883 Updates to the controls properties tree. This is a major update so there may be one or two 'old' refferences left. To simplify the transisition there is a file called README.properties in the docs-mini directory of FlightGear that explains the new controls layout. 2003-04-01 12:43:18 +00:00
david
c8b8722a14 Don't fiddle with control positions at startup -- we can do that in
the *-set.xml files if desired.
2003-03-02 02:22:18 +00:00
david
c7998b9940 Initialize speed from mach number or vcas more-or-less properly. 2003-03-02 01:44:11 +00:00
david
1e5d48d1d9 Add spdFromMach() and spdFromVCAS(). 2003-03-02 01:43:39 +00:00
david
c07f22ea16 Begin supporting a starting speed for YASim:
- NED and UVW are working correctly
- knots is giving true airspeed instead of calibrated airspeed
- mach is not working at all

This desperately needs a trimming routine.
2003-02-22 20:29:43 +00:00
david
8eac88efe9 Fixed calibrated airspeed output so that it accounts for wind. 2003-02-19 17:41:53 +00:00
david
b78d5a0b93 Interpolate the twist linearly over the wing.
Reduce the minimum number of twist segments from 16 to 8.
2003-02-18 17:37:28 +00:00
david
7228024ed5 Added a "twist" attribute for wings to allow for washout (or washin,
if desired) in the stall.  This allows for fairly docile stalls when
desired, as on trainers (you also need to limit the elevator lift).
2003-02-18 16:50:07 +00:00
andy
ba84ec24bf Changing the thresholds to be bigger in the previous patch isn't
really useful unless we simultaneously change the per-iteration deltas
to be smaller.  Add another pseudo-tunable to control the speed with
which we change values across iterations.  As it turns out, this is
much more effective than the threshold tunable.  It does come at the
cost of lower solution performance, however.
2002-12-12 02:15:06 +00:00
andy
ac93c22545 Put in some (currently compile-time) tuning for the solver threshold.
A recent change resulted in the Piper Cub oscillating about its
correct solution.
2002-12-11 22:58:47 +00:00
andy
4fb6673ff7 Update masses on the rigid body when consuming fuel. Simply updating
the tank capacity won't change the aircraft.
2002-12-11 22:52:52 +00:00
david
2e8572a4c5 Ignore more generated files. 2002-12-04 01:01:45 +00:00
andy
d98b7f05ff Honor the /sim/freeze/fuel property to inhibit fuel consumption at runtime.
Link the standalone executable against the source files explicitly rather
than libYASim, as the Irix linker can't handle the unneeded dependance on
other parts of FlightGear.
2002-11-30 20:22:25 +00:00
andy
0b2a45e256 Add the command-line yasim compiler to the automake configuration. It
installs into the build directory as "yasim".  Simply run it with the
xml file as its only argument.
2002-11-30 06:28:18 +00:00
andy
388d714fdc Fuel consumption. Simple implementation without support for tank selection
or engine-specific feeds.
2002-11-30 06:12:20 +00:00
andy
fe4e83a10b Added a tunable "induced drag" number to aircraft. One of the things that
isn't well-constrained by the solution process is the drag-vs-aoa curve.
The default value that YASim picked was very steep, and resulted in most
of the jets flying their approaches *way* behind the power curve.  This
changes the default to be more forgiving, and adds an "idrag" tunable
to the configuration file for tweakers.

Also, change the default gear springiness to be less stiff.
2002-11-30 02:24:16 +00:00
andy
e8e1a087fe Add "spring" and "damp" tunables to gear objects. 2002-11-09 21:08:10 +00:00
andy
7b7de3d3e0 Blindingly stupid ground effect bug. It interpolated in the wrong direction
(zero at ground, maximum at 1-span!)
2002-11-05 21:36:47 +00:00
david
2bc7a538cf Eliminate dependency of flight.hxx on model.hxx, to avoid unnecessary
rebuilding.
2002-11-03 15:41:30 +00:00
andy
f80b8660bf Fix coordinate conventions for reporting pilot acceleration. Add a few
digits to the c.g. report.
2002-10-27 04:30:34 +00:00
curt
4f00d9a959 Tidy up the autoconf/automake configuration a bit.
- Removed some old cruft.

- Removed some support for older versions of automake which technically was
  correct, but caused the newer automakes to squawk warnings during an
  initial sanity check (which isn't done very intelligently.)

  NOTE: this fix is technically not correct for older version of automake.
  These older version use the variable "INCLUDES" internally and could have
  them already set to an important value.  That is why we were appending
  our values to them.  However, newer versions of automake don't set this
  value themselves so it is an error to append to a non-existant variable.
  We seem to "get away" with overwriting the value on older versions of
  automake, but if you have problems, consider upgrading to at least
  automake-1.5.
2002-08-25 19:40:04 +00:00
david
c3f4b63258 Remove dependency on acmodel.hxx out of flight.hxx (which is included
many places) and into the files that actually use it.
2002-08-07 01:30:21 +00:00
andy
b162cf8707 Wrong units when interpreting <weight> tags. 2002-06-24 04:18:53 +00:00
andy
8199ece7dc Hack in an /accelerations/pilot-g property, for testing a new panel
instrument.  This needs to move somewhere permanent.

Also, remove a bogus fuel consumption setting that (1) was off by a factor
of 3600 (hours, not seconds) and (2) collided with identical code in FGFDM.
2002-06-20 04:11:19 +00:00
andy
9541e06a1e Finally fixed the flap drag issue. Drag modifications need to be based on
the amount of drag that the produced lift *would* have produced given an
unflapped air surface.  A nifty trick involving the assumption that AoA is
small works for this, and produces plausible results in the high AoA case
as well.

Also, trim for approach using the elevator-trim control, not elevator.
Just cosmetic for current planes, but future ones might have differing
implementations of trim.
2002-06-15 05:40:02 +00:00
andy
a682823ada Bugfix. The engine thrust is recalculated based on the current N1 value
(and not the throttle setting), but the recalculation left in a degeneracy
when the target/throttle setting was exactly zero.  Zero times a big number
is still zero.  Fixed to use real math, not theoretical math.
2002-06-12 08:23:05 +00:00
andy
df2b147ef5 Really simple command line airplane compiler. Basically a test program;
not integrated into the Makefile.am stuff.
2002-06-10 20:15:35 +00:00
andy
0cabedaa4f Use the density values from the environment subsystem, to properly handle
density variations due to humidity.
2002-06-10 08:47:29 +00:00
andy
2852f27bdc Uninitialized data problem. As it turns out, this never bit us because
the _chord member is only used uninitialized in circumstances where the
result is thrown away.  Still, bad practice.  Found with valgrind.
2002-06-04 07:23:34 +00:00