/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 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 #endif #include #include #include "FGConfigFile.h" #include "FGTable.h" #include "FGJSBBase.h" #include "FGPropertyManager.h" /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% DEFINITIONS %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/ #define ID_COEFFICIENT "$Id$" using std::vector; /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 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 [use "class documentation" below for API docs] %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% Note that the coefficients need not be calculated each delta-t. This is something that may be fixed someday. %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% CLASS DOCUMENTATION %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/ /** This class models the stability derivative coefficient lookup tables. Each coefficient for an axis is stored in that axes' vector of coefficients. Each FDM execution frame the Run() method of the [currently] FGAircraft model is called and the coefficient value is calculated. @author Jon S. Berndt @version $Id$ @see - */ /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% CLASS DECLARATION %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/ class FGCoefficient : public FGJSBBase { public: FGCoefficient(FGFDMExec*); virtual ~FGCoefficient(); virtual bool Load(FGConfigFile* AC_cfg); typedef vector MultVec; virtual double TotalValue(void); virtual inline double GetValue(void) const { return totalValue; } virtual inline string Getname(void) const {return name;} virtual inline double GetSD(void) const { return SD;} inline MultVec Getmultipliers(void) {return multipliers;} void DumpSD(void); /** Outputs coefficient information. Non-dimensionalizing parameter descriptions are output for each aero coefficient defined. @param multipliers the list of multipliers for this coefficient.*/ virtual void DisplayCoeffFactors(void); virtual inline string GetCoefficientStrings(void) { return name; } virtual string GetCoefficientValues(void); inline void setBias(double b) { bias=b; } inline void setGain(double g) { gain=g; }; inline double getBias(void) const { return bias; } inline double getGain(void) const { return gain; } virtual void bind(FGPropertyManager *parent); virtual void unbind(void); private: enum Type {UNKNOWN, VALUE, VECTOR, TABLE, EQUATION}; int numInstances; string filename; string description; string name; string method; string multparms; string multparmsRow; string multparmsCol; double Value(double, double); double Value(double); double Value(void); double StaticValue; double totalValue; double bias,gain; FGPropertyManager *LookupR, *LookupC; FGPropertyManager *node; MultVec multipliers; int rows, columns; Type type; double SD; // Actual stability derivative (or other coefficient) value FGTable *Table; FGFDMExec* FDMExec; FGState* State; FGAtmosphere* Atmosphere; FGFCS* FCS; FGAircraft* Aircraft; FGTranslation* Translation; FGRotation* Rotation; FGPosition* Position; FGAuxiliary* Auxiliary; FGOutput* Output; FGPropertyManager* PropertyManager; virtual void Debug(int from); }; //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% #endif