/************************************************************************** * 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 #include "slew.h" #include "../flight.h" #include "../../Aircraft/aircraft.h" #include "../../Controls/controls.h" #include "../../constants.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 = ¤t_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 = ¤t_aircraft.flight; c = ¤t_aircraft.controls; /* f->Psi += ( c->aileron / 8 ); if ( f->Psi > FG_2PI ) { f->Psi -= FG_2PI; } else if ( f->Psi < 0 ) { f->Psi += FG_2PI; } 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 1.5 1997/07/19 22:35:06 curt /* Moved fiddled with PI to avoid compiler warnings. /* * Revision 1.4 1997/06/21 17:12:51 curt * Capitalized subdirectory names. * * 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. * */