From: curt Date: Sat, 31 May 1997 19:24:04 +0000 (+0000) Subject: Initial revision. X-Git-Url: https://git.mxchange.org/?a=commitdiff_plain;h=607546e8f41ef530af21712f740b717553951eb6;p=flightgear.git Initial revision. --- diff --git a/Controls/controls.c b/Controls/controls.c new file mode 100644 index 000000000..7d882c0f6 --- /dev/null +++ b/Controls/controls.c @@ -0,0 +1,173 @@ +/************************************************************************** + * controls.c -- defines a standard interface to all flight sim controls + * + * 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 "controls.h" +#include "../aircraft/aircraft.h" + + +void fgControlsInit() { + int i; + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Elevator = 0.0; + FG_Elev_Trim = 1.969572E-03; + FG_Aileron = 0.0; + FG_Rudder = 0.0; + + for ( i = 0; i < FG_MAX_ENGINES; i++ ) { + FG_Throttle[i] = 0.0; + } + +} + + +void fgElevMove(double amt) { + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Elevator += amt; + + if ( FG_Elevator < -1.0 ) FG_Elevator = -1.0; + if ( FG_Elevator > 1.0 ) FG_Elevator = 1.0; +} + +void fgElevSet(double pos) { + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Elevator = pos; + + if ( FG_Elevator < -1.0 ) FG_Elevator = -1.0; + if ( FG_Elevator > 1.0 ) FG_Elevator = 1.0; +} + +void fgElevTrimMove(double amt) { + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Elev_Trim += amt; + + if ( FG_Elev_Trim < -1.0 ) FG_Elev_Trim = -1.0; + if ( FG_Elev_Trim > 1.0 ) FG_Elev_Trim = 1.0; +} + +void fgElevTrimSet(double pos) { + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Elev_Trim = pos; + + if ( FG_Elev_Trim < -1.0 ) FG_Elev_Trim = -1.0; + if ( FG_Elev_Trim > 1.0 ) FG_Elev_Trim = 1.0; +} + +void fgAileronMove(double amt) { + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Aileron += amt; + + if ( FG_Aileron < -1.0 ) FG_Aileron = -1.0; + if ( FG_Aileron > 1.0 ) FG_Aileron = 1.0; +} + +void fgAileronSet(double pos) { + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Aileron = pos; + + if ( FG_Aileron < -1.0 ) FG_Aileron = -1.0; + if ( FG_Aileron > 1.0 ) FG_Aileron = 1.0; +} + +void fgRudderMove(double amt) { + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Rudder += amt; + + if ( FG_Rudder < -1.0 ) FG_Rudder = -1.0; + if ( FG_Rudder > 1.0 ) FG_Rudder = 1.0; +} + +void fgRudderSet(double pos) { + struct control_params *c; + c = ¤t_aircraft.controls; + + FG_Rudder = pos; + + if ( FG_Rudder < -1.0 ) FG_Rudder = -1.0; + if ( FG_Rudder > 1.0 ) FG_Rudder = 1.0; +} + +void fgThrottleMove(int engine, double amt) { + int i; + struct control_params *c; + c = ¤t_aircraft.controls; + + if ( engine == FG_Throttle_All ) { + for ( i = 0; i < FG_MAX_ENGINES; i++ ) { + FG_Throttle[i] += amt; + if ( FG_Throttle[i] < 0.0 ) FG_Throttle[i] = 0.0; + if ( FG_Throttle[i] > 1.0 ) FG_Throttle[i] = 1.0; + } + } else { + if ( (engine >= 0) && (engine < FG_MAX_ENGINES) ) { + FG_Throttle[engine] += amt; + if ( FG_Throttle[engine] < 0.0 ) FG_Throttle[engine] = 0.0; + if ( FG_Throttle[engine] > 1.0 ) FG_Throttle[engine] = 1.0; + } + } +} + +void fgThrottleSet(int engine, double pos) { + int i; + struct control_params *c; + c = ¤t_aircraft.controls; + + if ( engine == FG_Throttle_All ) { + for ( i = 0; i < FG_MAX_ENGINES; i++ ) { + FG_Throttle[i] = pos; + if ( FG_Throttle[i] < 0.0 ) FG_Throttle[i] = 0.0; + if ( FG_Throttle[i] > 1.0 ) FG_Throttle[i] = 1.0; + } + } else { + if ( (engine >= 0) && (engine < FG_MAX_ENGINES) ) { + FG_Throttle[engine] = pos; + if ( FG_Throttle[engine] < 0.0 ) FG_Throttle[engine] = 0.0; + if ( FG_Throttle[engine] > 1.0 ) FG_Throttle[engine] = 1.0; + } + } +} + + +/* $Log$ +/* Revision 1.1 1997/05/31 19:24:04 curt +/* Initial revision. +/* + */