/******************************************************************************* 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 STL_STRING FG_USING_STD(string); #else # include #endif #include #include "FGConfigFile.h" #include "FGDefs.h" /******************************************************************************* DEFINES *******************************************************************************/ using namespace std; /******************************************************************************* 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_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 *******************************************************************************/ class FGCoefficient { public: FGCoefficient(FGFDMExec*, FGConfigFile*); ~FGCoefficient(void); bool Allocate(int); bool Allocate(int, int); float Value(float, float); float Value(float); float Value(void); float TotalValue(void); 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;} inline long int Getmultipliers(void) {return multipliers;} void DumpSD(void); enum Type {UNKNOWN, VALUE, VECTOR, TABLE, EQUATION}; protected: private: int numInstances; string filename; string description; string name; string method; float StaticValue; float *Table2D; float **Table3D; float LookupR, LookupC; long int multipliers; long int mult_idx[10]; int rows, columns; Type type; int mult_count; float SD; // Actual stability derivative (or other coefficient) value FGFDMExec* FDMExec; FGState* State; FGAtmosphere* Atmosphere; FGFCS* FCS; FGAircraft* Aircraft; FGTranslation* Translation; FGRotation* Rotation; FGPosition* Position; FGAuxiliary* Auxiliary; FGOutput* Output; }; /******************************************************************************/ #endif