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flightgear/src/FDM/UIUCModel/uiuc_controlInput.cpp

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2000-09-06 19:52:37 +00:00
/**********************************************************************
FILENAME: uiuc_controlInput.cpp
----------------------------------------------------------------------
DESCRIPTION: sets control surface deflections for specified input
modes
----------------------------------------------------------------------
STATUS: alpha version
----------------------------------------------------------------------
REFERENCES:
----------------------------------------------------------------------
HISTORY: 04/08/2000 initial release
----------------------------------------------------------------------
AUTHOR(S): Jeff Scott <jscott@mail.com>
----------------------------------------------------------------------
VARIABLES:
----------------------------------------------------------------------
INPUTS: -Simtime
-deflection times
-deflection angles
----------------------------------------------------------------------
OUTPUTS: -elevator deflection
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CALLED BY: uiuc_coefficients.cpp
----------------------------------------------------------------------
CALLS TO: none
----------------------------------------------------------------------
COPYRIGHT: (C) 2000 by Michael Selig
This program is free software; you can redistribute it and/or
modify it under the terms of the GNU General Public License
as published by the Free Software Foundation.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program; if not, write to the Free Software
Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307,
USA or view http://www.gnu.org/copyleft/gpl.html.
**********************************************************************/
#include "uiuc_controlInput.h"
#include <iostream.h>
void uiuc_controlInput()
{
// elevator step input
if (elevator_step)
{
if (Simtime >= elevator_step_startTime)
{
elevator = elevator + elevator_step_angle;
}
}
// elevator singlet input
if (elevator_singlet)
{
if (Simtime >= elevator_singlet_startTime &&
Simtime <= (elevator_singlet_startTime + elevator_singlet_duration))
{
elevator = elevator + elevator_singlet_angle;
}
}
// elevator doublet input
if (elevator_doublet)
{
if (Simtime >= elevator_doublet_startTime &&
Simtime <= (elevator_doublet_startTime + elevator_doublet_duration/2))
{
elevator = elevator + elevator_doublet_angle;
}
else if (Simtime >= (elevator_doublet_startTime + elevator_doublet_duration/2) &&
Simtime <= (elevator_doublet_startTime + elevator_doublet_duration))
{
elevator = elevator - elevator_doublet_angle;
}
}
// elevator input
if (elevator_input)
{
double elevator_input_endTime = elevator_input_timeArray[elevator_input_ntime];
if (Simtime >= elevator_input_startTime &&
Simtime <= (elevator_input_startTime + elevator_input_endTime))
{
double time = Simtime - elevator_input_startTime;
elevator = elevator +
uiuc_1Dinterpolation(elevator_input_timeArray,
elevator_input_deArray,
elevator_input_ntime,
time);
}
}
return;
}
// end uiuc_controlInput.cpp