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flightgear/Slew/slew.c

108 lines
2.8 KiB
C

/**************************************************************************
* slew.c -- the "slew" flight model
*
* Written by Curtis Olson, started May 1997.
*
* Copyright (C) 1997 Curtis L. Olson - curt@infoplane.com
*
* 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; either version 2 of the
* License, or (at your option) any later version.
*
* 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., 675 Mass Ave, Cambridge, MA 02139, USA.
*
* $Id$
* (Log is kept at end of this file)
**************************************************************************/
#include <math.h>
#include "slew.h"
#include "../flight.h"
#include "../../aircraft/aircraft.h"
#include "../../controls/controls.h"
#ifndef M_PI
#define M_PI 3.14159265358979323846 /* pi */
#endif
#ifndef PI2
#define PI2 (M_PI + M_PI)
#endif
/* reset flight params to a specific position */
void fgSlewInit(double pos_x, double pos_y, double pos_z, double heading) {
struct flight_params *f;
f = &current_aircraft.flight;
/* f->pos_x = pos_x;
f->pos_y = pos_y;
f->pos_z = pos_z;
f->vel_x = 0.0;
f->vel_y = 0.0;
f->vel_z = 0.0;
f->Phi = 0.0;
f->Theta = 0.0;
f->Psi = 0.0;
f->vel_Phi = 0.0;
f->vel_Theta = 0.0;
f->vel_Psi = 0.0;
f->Psi = heading; */
}
/* update position based on inputs, positions, velocities, etc. */
void fgSlewUpdate() {
struct flight_params *f;
struct control_params *c;
f = &current_aircraft.flight;
c = &current_aircraft.controls;
/* f->Psi += ( c->aileron / 8 );
if ( f->Psi > PI2 ) {
f->Psi -= PI2;
} else if ( f->Psi < 0 ) {
f->Psi += PI2;
}
f->vel_x = -c->elev;
f->pos_x = f->pos_x + (cos(f->Psi) * f->vel_x);
f->pos_y = f->pos_y + (sin(f->Psi) * f->vel_x); */
}
/* $Log$
/* Revision 1.3 1997/05/29 22:40:00 curt
/* Working on incorporating the LaRCsim flight model.
/*
* Revision 1.2 1997/05/29 12:30:19 curt
* Some initial mods to work better in a timer environment.
*
* Revision 1.1 1997/05/29 02:29:42 curt
* Moved to their own directory.
*
* Revision 1.2 1997/05/23 15:40:37 curt
* Added GNU copyright headers.
*
* Revision 1.1 1997/05/16 16:04:45 curt
* Initial revision.
*
*/