flightgear/src/FDM/JSBSim/FGRotation.h

/*******************************************************************************

 Header:       FGRotation.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 FGROTATION_H
#define FGROTATION_H

/*******************************************************************************
INCLUDES
*******************************************************************************/

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

#ifndef M_PI
#  include <simgear/constants.h>
#  define M_PI FG_PI
#endif

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

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

class FGRotation : public FGModel
{
  FGColumnVector vPQR;
  FGColumnVector vPQRdot;
  FGColumnVector vMoments;
  FGColumnVector vEuler;

  float Ixx, Iyy, Izz, Ixz;
  float dt;

  void GetState(void);

public:
  FGRotation(FGFDMExec*);
  ~FGRotation(void);

  bool Run(void);

  inline FGColumnVector GetPQR(void) {return vPQR;}
  inline FGColumnVector GetPQRdot(void) {return vPQRdot;}
  inline FGColumnVector GetEuler(void) {return vEuler;}
  inline void SetPQR(FGColumnVector tt) {vPQR = tt;}
  inline void SetEuler(FGColumnVector tt) {vEuler = tt;}
  inline float Getphi(void) {return vEuler(1);}
  inline float Gettht(void) {return vEuler(2);}
  inline float Getpsi(void) {return vEuler(3);}
};

/******************************************************************************/
#endif