/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 Header:       FGTranslation.h
 Author:       Jon Berndt
 Date started: 12/02/98
 
 ------------- 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
--------------------------------------------------------------------------------
12/02/98   JSB   Created
 
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
COMMENTS, REFERENCES,  and NOTES
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
[1] Cooke, Zyda, Pratt, and McGhee, "NPSNET: Flight Simulation Dynamic Modeling
    Using Quaternions", Presence, Vol. 1, No. 4, pp. 404-420  Naval Postgraduate
    School, January 1994
[2] D. M. Henderson, "Euler Angles, Quaternions, and Transformation Matrices",
    JSC 12960, July 1977
[3] Richard E. McFarland, "A Standard Kinematic Model for Flight Simulation at
    NASA-Ames", NASA CR-2497, January 1975
[4] Barnes W. McCormick, "Aerodynamics, Aeronautics, and Flight Mechanics",
    Wiley & Sons, 1979 ISBN 0-471-03032-5
[5] Bernard Etkin, "Dynamics of Flight, Stability and Control", Wiley & Sons,
    1982 ISBN 0-471-08936-2
 
  The order of rotations used in this class corresponds to a 3-2-1 sequence,
  or Y-P-R, or Z-Y-X, if you prefer.
 
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
SENTRY
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

#ifndef FGTRANSLATION_H
#define FGTRANSLATION_H

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
INCLUDES
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

#ifdef FGFS
#  include <simgear/compiler.h>
#  ifdef SG_HAVE_STD_INCLUDES
#    include <cmath>
#  else
#    include <math.h>
#  endif
#else
#  include <cmath>
#endif

#include "FGModel.h"
#include "FGMatrix.h"

#define ID_TRANSLATION "$Id$"

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS DECLARATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

class FGTranslation : public FGModel {
public:
  FGTranslation(FGFDMExec*);
  ~FGTranslation();

  inline FGColumnVector GetUVW   (void)    { return vUVW; }
  inline float          GetUVW   (int idx) { return vUVW(idx); }
  inline FGColumnVector GetUVWdot(void)    { return vUVWdot; }
  inline float          GetUVWdot(int idx) { return vUVWdot(idx); }
  inline FGColumnVector GetNcg   (void)    { return vNcg; }
  inline float          GetNcg   (int idx) { return vNcg(idx); }
  inline FGColumnVector GetvAero (void)    { return vAero; }
  inline float          GetvAero (int idx) { return vAero(idx); }

  inline float Getalpha(void) { return alpha; }
  inline float Getbeta (void) { return beta; }
  inline float Getqbar (void) { return qbar; }
  inline float GetVt   (void) { return Vt; }
  inline float GetMach (void) { return Mach; }
  inline float Getadot (void) { return adot; }
  inline float Getbdot (void) { return bdot; }

  void SetUVW(FGColumnVector tt) { vUVW = tt; }

  inline void Setalpha(float tt) { alpha = tt; }
  inline void Setbeta (float tt) { beta  = tt; }
  inline void Setqbar (float tt) { qbar = tt; }
  inline void SetVt   (float tt) { Vt = tt; }
  inline void SetMach (float tt) { Mach=tt; }
  inline void Setadot (float tt) { adot = tt; }
  inline void Setbdot (float tt) { bdot = tt; }

  inline void SetAB(float t1, float t2) { alpha=t1; beta=t2; }
  
  bool Run(void);

protected:

private:
  FGColumnVector vUVW;
  FGColumnVector vUVWdot;
  FGColumnVector vNcg;
  FGColumnVector vPQR;
  FGColumnVector vForces;
  FGColumnVector vEuler;
  FGColumnVector vlastUVWdot;
  FGMatrix       mVel;
  FGColumnVector vAero;

  float Vt, qbar, Mach;
  float Mass, dt;
  float alpha, beta;
  float adot,bdot;
  float rho;

  void GetState(void);
  void Debug(void);
};

//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#endif