1998-10-17 01:33:52 +00:00
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// slew.cxx -- the "slew" flight model
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//
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// Written by Curtis Olson, started May 1997.
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//
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// Copyright (C) 1997 Curtis L. Olson - curt@infoplane.com
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//
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// This program is free software; you can redistribute it and/or
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// modify it under the terms of the GNU General Public License as
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// published by the Free Software Foundation; either version 2 of the
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// License, or (at your option) any later version.
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//
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// This program is distributed in the hope that it will be useful, but
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// WITHOUT ANY WARRANTY; without even the implied warranty of
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// MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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// General Public License for more details.
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//
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// You should have received a copy of the GNU General Public License
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// along with this program; if not, write to the Free Software
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// Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
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//
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// $Id$
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1997-05-29 02:29:42 +00:00
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#include <math.h>
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1998-10-16 23:26:44 +00:00
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#include "slew.hxx"
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1999-02-01 21:33:23 +00:00
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#include <FDM/flight.hxx>
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1998-10-16 23:26:44 +00:00
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#include <Aircraft/aircraft.hxx>
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1998-10-17 01:33:52 +00:00
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#include <Controls/controls.hxx>
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1998-01-27 00:47:41 +00:00
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#include <Include/fg_constants.h>
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1997-05-29 02:29:42 +00:00
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1998-10-17 01:33:52 +00:00
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// reset flight params to a specific position
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1997-05-29 02:29:42 +00:00
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void fgSlewInit(double pos_x, double pos_y, double pos_z, double heading) {
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1999-02-05 21:28:09 +00:00
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FGInterface *f;
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1998-12-05 15:53:59 +00:00
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f = current_aircraft.fdm_state;
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1997-05-29 02:29:42 +00:00
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1998-01-19 18:40:15 +00:00
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/*
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f->pos_x = pos_x;
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1997-05-29 02:29:42 +00:00
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f->pos_y = pos_y;
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f->pos_z = pos_z;
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f->vel_x = 0.0;
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f->vel_y = 0.0;
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f->vel_z = 0.0;
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f->Phi = 0.0;
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f->Theta = 0.0;
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f->Psi = 0.0;
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f->vel_Phi = 0.0;
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f->vel_Theta = 0.0;
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f->vel_Psi = 0.0;
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1998-01-19 18:40:15 +00:00
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f->Psi = heading;
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*/
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1997-05-29 02:29:42 +00:00
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}
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1998-10-17 01:33:52 +00:00
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// update position based on inputs, positions, velocities, etc.
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1998-01-19 18:40:15 +00:00
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void fgSlewUpdate( void ) {
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1999-02-05 21:28:09 +00:00
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FGInterface *f;
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1998-12-05 16:13:10 +00:00
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FGControls *c;
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1997-05-29 02:29:42 +00:00
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1998-12-05 15:53:59 +00:00
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f = current_aircraft.fdm_state;
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1998-02-07 15:29:31 +00:00
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c = current_aircraft.controls;
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1997-05-29 02:29:42 +00:00
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1997-05-29 22:39:49 +00:00
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/* f->Psi += ( c->aileron / 8 );
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1997-07-19 22:35:06 +00:00
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if ( f->Psi > FG_2PI ) {
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f->Psi -= FG_2PI;
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1997-05-29 02:29:42 +00:00
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} else if ( f->Psi < 0 ) {
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1997-07-19 22:35:06 +00:00
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f->Psi += FG_2PI;
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1997-05-29 02:29:42 +00:00
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}
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f->vel_x = -c->elev;
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f->pos_x = f->pos_x + (cos(f->Psi) * f->vel_x);
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1997-05-29 22:39:49 +00:00
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f->pos_y = f->pos_y + (sin(f->Psi) * f->vel_x); */
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1997-05-29 02:29:42 +00:00
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}
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