/******************************************************************************* Header: FGState.h Author: Jon S. Berndt Date started: 11/17/98 ------------- 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. FUNCTIONAL DESCRIPTION -------------------------------------------------------------------------------- Based on Flightgear code, which is based on LaRCSim. This class wraps all global state variables (such as velocity, position, orientation, etc.). HISTORY -------------------------------------------------------------------------------- 11/17/98 JSB Created ******************************************************************************** SENTRY *******************************************************************************/ #ifndef FGSTATE_H #define FGSTATE_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 #include "FGDefs.h" #include "FGInitialCondition.h" #include "FGMatrix.h" /******************************************************************************* DEFINES *******************************************************************************/ using namespace std; /******************************************************************************* CLASS DECLARATION *******************************************************************************/ class FGFDMExec; class FGState { public: FGState(FGFDMExec*); ~FGState(void); bool Reset(string, string, string); void Initialize(float, float, float, float, float, float, float, float, float); void Initialize(FGInitialCondition *FGIC); bool StoreData(string); inline float Getadot(void) {return adot;} inline float Getbdot(void) {return bdot;} inline float GetLocalAltitudeOverRunway(void) {return LocalAltitudeOverRunway;} inline float Geta(void) {return a;} inline float Getsim_time(void) {return sim_time;} inline float Getdt(void) {return dt;} float GetParameter(int val_idx); float GetParameter(string val_string); int GetParameterIndex(string val_string); inline void Setadot(float tt) {adot = tt;} inline void Setbdot(float tt) {bdot = tt;} inline void SetLocalAltitudeOverRunway(float tt) {LocalAltitudeOverRunway = tt;} inline void Seta(float tt) {a = tt;} inline float Setsim_time(float tt) {sim_time = tt; return sim_time;} inline void Setdt(float tt) {dt = tt;} void SetParameter(int, float); inline float IncrTime(void) {sim_time+=dt;return sim_time;} void InitMatrices(float phi, float tht, float psi); void CalcMatrices(void); void IntegrateQuat(FGColumnVector vPQR, int rate); FGColumnVector CalcEuler(void); FGMatrix GetTs2b(float alpha, float beta); FGMatrix GetTl2b(void) {return mTl2b;} FGMatrix GetTb2l(void) {return mTb2l;} private: float adot, bdot; // alpha dot and beta dot float a; // speed of sound float sim_time, dt; FGFDMExec* FDMExec; float LocalAltitudeOverRunway; FGMatrix mTb2l; FGMatrix mTl2b; FGMatrix mTs2b; FGColumnVector vQtrn; typedef map CoeffMap; CoeffMap coeffdef; protected: enum {ePhi=1, eTht, ePsi}; enum {eP=1, eQ, eR}; }; /******************************************************************************/ #endif