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flightgear/Simulator/FDM/JSBsim/FGCoefficient.h
1999-06-21 03:01:57 +00:00

170 lines
4.6 KiB
C++

/*******************************************************************************
Header: FGCoefficient.h
Author: Jon Berndt
Date started: 12/28/98
------------- 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.
HISTORY
--------------------------------------------------------------------------------
12/28/98 JSB Created
********************************************************************************
SENTRY
*******************************************************************************/
#ifndef FGCOEFFICIENT_H
#define FGCOEFFICIENT_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 <map>
/*******************************************************************************
DEFINES
*******************************************************************************/
using namespace std;
#define FG_QBAR 1
#define FG_WINGAREA 2
#define FG_WINGSPAN 4
#define FG_CBAR 8
#define FG_ALPHA 16
#define FG_ALPHADOT 32
#define FG_BETA 64
#define FG_BETADOT 128
#define FG_PITCHRATE 256
#define FG_ROLLRATE 512
#define FG_YAWRATE 1024
#define FG_ELEVATOR 2048
#define FG_AILERON 4096
#define FG_RUDDER 8192
#define FG_MACH 16384
#define FG_ALTITUDE 32768L
#define FG_I2VEL 65536L
/*******************************************************************************
FORWARD DECLARATIONS
*******************************************************************************/
class FGFDMExec;
class FGState;
class FGAtmosphere;
class FGFCS;
class FGAircraft;
class FGTranslation;
class FGRotation;
class FGPosition;
class FGAuxiliary;
class FGOutput;
/*******************************************************************************
COMMENTS, REFERENCES, and NOTES
********************************************************************************
This class models the stability derivative coefficient lookup tables or
equations. Note that the coefficients need not be calculated each delta-t.
FG_QBAR 1
FG_WINGAREA 2
FG_WINGSPAN 4
FG_CBAR 8
FG_ALPHA 16
FG_ALPHADOT 32
FG_BETA 64
FG_BETADOT 128
FG_PITCHRATE 256
FG_ROLLRATE 512
FG_YAWRATE 1024
FG_ELEVATOR 2048
FG_AILERON 4096
FG_RUDDER 8192
FG_MACH 16384
FG_ALTITUDE 32768L
FG_I2VEL 65536L
********************************************************************************
CLASS DECLARATION
*******************************************************************************/
class FGCoefficient
{
public:
FGCoefficient(FGFDMExec*, ifstream&);
~FGCoefficient(void);
bool Allocate(int);
bool Allocate(int, int);
float Value(float, float);
float Value(float);
float Value(void);
float TotalValue(void);
enum Type {UNKNOWN, VALUE, VECTOR, TABLE, EQUATION};
protected:
private:
typedef map<string, long> CoeffMap;
CoeffMap coeffdef;
string filename;
string description;
string name;
string method;
float StaticValue;
float *Table2D;
float **Table3D;
float LookupR, LookupC;
long int mult_idx[10];
int rows, columns;
Type type;
int multipliers;
int mult_count;
float GetCoeffVal(int);
FGFDMExec* FDMExec;
FGState* State;
FGAtmosphere* Atmosphere;
FGFCS* FCS;
FGAircraft* Aircraft;
FGTranslation* Translation;
FGRotation* Rotation;
FGPosition* Position;
FGAuxiliary* Auxiliary;
FGOutput* Output;
};
/******************************************************************************/
#endif