/******************************************************************************* 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 # ifdef FG_HAVE_STD_INCLUDES # include # else # include # endif FG_USING_STD(string); #else # include # include #endif #include /******************************************************************************* 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_BI2VEL 65536L #define FG_CI2VEL 131072L /******************************************************************************* 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_BI2VEL 65536L FG_CI2VEL 131072L ******************************************************************************** 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 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