1
0
Fork 0
flightgear/JSBsim/FGState.h

140 lines
4.3 KiB
C
Raw Normal View History

1999-02-05 21:26:01 +00:00
/*******************************************************************************
Header: FGState.h
Author: Jon S. Berndt
Date started: 11/17/98
------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------
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., 59 Temple
Place - Suite 330, Boston, MA 02111-1307, USA.
Further information about the GNU General Public License can also be found on
the world wide web at http://www.gnu.org.
FUNCTIONAL DESCRIPTION
--------------------------------------------------------------------------------
Based on Flightgear code, which is based on LaRCSim. This class wraps all
global state variables (such as velocity, position, orientation, etc.).
HISTORY
--------------------------------------------------------------------------------
11/17/98 JSB Created
********************************************************************************
1999-02-05 21:26:01 +00:00
SENTRY
*******************************************************************************/
#ifndef FGSTATE_H
#define FGSTATE_H
/*******************************************************************************
INCLUDES
*******************************************************************************/
#ifdef FGFS
# include <Include/compiler.h>
# include STL_STRING
# ifdef FG_HAVE_STD_INCLUDES
# include <fstream>
# else
# include <fstream.h>
# endif
FG_USING_STD(string);
#else
# include <string>
# include <fstream>
#endif
#include "FGDefs.h"
1999-02-05 21:26:01 +00:00
/*******************************************************************************
DEFINES
*******************************************************************************/
/*******************************************************************************
CLASS DECLARATION
*******************************************************************************/
class FGFDMExec;
1999-02-05 21:26:01 +00:00
class FGState
{
public:
FGState(FGFDMExec*);
1999-02-05 21:26:01 +00:00
~FGState(void);
bool Reset(string, string);
bool StoreData(string);
bool DumpData(string);
1999-02-05 21:26:01 +00:00
bool DisplayData(void);
inline float GetVt(void) {return Vt;}
inline float Getlatitude(void) {return latitude;}
inline float Getlongitude(void) {return longitude;}
inline float GetGeodeticLat(void) {return GeodeticLat;}
inline float Getadot(void) {return adot;}
inline float Getbdot(void) {return bdot;}
inline float Geth(void) {return h;}
inline float Geta(void) {return a;}
inline float GetMach(void) {return Mach;}
1999-02-05 21:26:01 +00:00
inline float Getsim_time(void) {return sim_time;}
inline float Getdt(void) {return dt;}
inline float Getqbar(void) {return qbar;}
inline void SetVt(float tt) {Vt = tt;}
inline void Setlatitude(float tt) {latitude = tt;}
inline void Setlongitude(float tt) {longitude = tt;}
inline void SetGeodeticLat(float tt) {GeodeticLat = tt;}
inline void Setadot(float tt) {adot = tt;}
inline void Setbdot(float tt) {bdot = tt;}
inline void Setqbar(float tt) {qbar = tt;}
inline void Seth(float tt) {h = tt;}
inline void Seta(float tt) {a = tt;}
inline void SetMach(float tt) {Mach = tt;}
inline float Setsim_time(float tt) {sim_time = tt; return sim_time;}
inline void Setdt(float tt) {dt = tt;}
1999-02-05 21:26:01 +00:00
inline float IncrTime(void) {sim_time+=dt;return sim_time;}
private:
float Vt; // Total velocity
float latitude, longitude; // position
float GeodeticLat; // Geodetic Latitude
float adot, bdot; // alpha dot and beta dot
float h, a; // altitude above sea level, speed of sound
float qbar; // dynamic pressure
1999-02-05 21:26:01 +00:00
float sim_time, dt;
float Mach; // Mach number
FGFDMExec* FDMExec;
1999-02-05 21:26:01 +00:00
protected:
1999-02-05 21:26:01 +00:00
};
/******************************************************************************/
#endif