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flightgear/src/FDM/JSBSim/FGCoefficient.h

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/*******************************************************************************
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
********************************************************************************
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SENTRY
*******************************************************************************/
#ifndef FGCOEFFICIENT_H
#define FGCOEFFICIENT_H
/*******************************************************************************
INCLUDES
*******************************************************************************/
#ifdef FGFS
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# include <simgear/compiler.h>
#endif
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#include <string>
#include <map>
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#include "FGConfigFile.h"
#include "FGDefs.h"
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/*******************************************************************************
DEFINES
*******************************************************************************/
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/*******************************************************************************
FORWARD DECLARATIONS
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*******************************************************************************/
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.
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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_MACH 2048
FG_ALTITUDE 4096
FG_BI2VEL 8192
FG_CI2VEL 16384
FG_ELEVATOR_POS 32768L
FG_AILERON_POS 65536L
FG_RUDDER_POS 131072L
FG_SPDBRAKE_POS 262144L
FG_FLAPS_POS 524288L
FG_ELEVATOR_CMD 1048576L
FG_AILERON_CMD 2097152L
FG_RUDDER_CMD 4194304L
FG_SPDBRAKE_CMD 8388608L
FG_FLAPS_CMD 16777216L
FG_SPARE1 33554432L
FG_SPARE2 67108864L
FG_SPARE3 134217728L
FG_SPARE4 268435456L
FG_SPARE5 536870912L
FG_SPARE6 1073741824L
The above definitions are found in FGDefs.h
********************************************************************************
CLASS DECLARATION
*******************************************************************************/
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class FGCoefficient
{
public:
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FGCoefficient(FGFDMExec*, FGConfigFile*);
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~FGCoefficient(void);
bool Allocate(int);
bool Allocate(int, int);
float Value(float, float);
float Value(float);
float Value(void);
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float TotalValue(void);
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inline string Getname(void) {return name;}
inline float GetSD(void) {return SD;}
// inline float GetSDValue(void) {return SD;}
// inline void SetSDValue(float tt) {SD = tt;}
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inline long int Getmultipliers(void) {return multipliers;}
void DumpSD(void);
enum Type {UNKNOWN, VALUE, VECTOR, TABLE, EQUATION};
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protected:
private:
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int numInstances;
string filename;
string description;
string name;
string method;
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float StaticValue;
float *Table2D;
float **Table3D;
float LookupR, LookupC;
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long int multipliers;
long int mult_idx[10];
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int rows, columns;
Type type;
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int mult_count;
float SD; // Actual stability derivative (or other coefficient) value
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FGFDMExec* FDMExec;
FGState* State;
FGAtmosphere* Atmosphere;
FGFCS* FCS;
FGAircraft* Aircraft;
FGTranslation* Translation;
FGRotation* Rotation;
FGPosition* Position;
FGAuxiliary* Auxiliary;
FGOutput* Output;
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};
/******************************************************************************/
#endif