/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

 Header:       FGAircraft.h
 Author:       Jon S. Berndt
 Date started: 12/12/98

 ------------- 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 Lesser 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 Lesser General Public License for more
 details.

 You should have received a copy of the GNU Lesser 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 Lesser General Public License can also be found on
 the world wide web at http://www.gnu.org.

HISTORY
--------------------------------------------------------------------------------
12/12/98   JSB   Created

%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
SENTRY
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

#ifndef FGAIRCRAFT_H
#define FGAIRCRAFT_H

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

#include <vector>

#include "FGModel.h"
#include <input_output/FGXMLElement.h>
#include <math/FGColumnVector3.h>

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
DEFINITIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

#define ID_AIRCRAFT "$Id: FGAircraft.h,v 1.5 2008/07/22 08:49:16 ehofman Exp $"

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FORWARD DECLARATIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

namespace JSBSim {

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS DOCUMENTATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/

/** Encapsulates an Aircraft and its systems.
<p> Owns all the parts (other classes) which make up this aircraft. This includes
    the Engines, Tanks, Propellers, Nozzles, Aerodynamic and Mass properties,
    landing gear, etc. These constituent parts may actually run as separate
    JSBSim models themselves, but the responsibility for initializing them and
    for retrieving their force and moment contributions falls to FGAircraft.
<p> The \<metrics> section of the aircraft configuration file is read here, and
    the metrical information is held by this class.
<h3>Configuration File Format for \<metrics> Section:</h3>
@code
    <metrics>
        <wingarea unit="{FT2 | M2}"> {number} </wingarea>
        <wingspan unit="{FT | M}"> {number} </wingspan>
        <chord unit="{FT | M}"> {number} </chord>
        <htailarea unit="{FT2 | M2}"> {number} </htailarea>
        <htailarm unit="{FT | M}"> {number} </htailarm>
        <vtailarea unit="{FT2 | M}"> {number} </vtailarea>
        <vtailarm unit="{FT | M}"> {number} </vtailarm>
        <wing_incidence unit="{RAD | DEG}"> {number} </wing_incidence>
        <location name="{AERORP | EYEPOINT | VRP}" unit="{IN | M}">
            <x> {number} </x>
            <y> {number} </y>
            <z> {number} </z>
        </location>
        {other location blocks}
    </metrics>
@endcode

    @author Jon S. Berndt
    @version $Id: FGAircraft.h,v 1.5 2008/07/22 08:49:16 ehofman Exp $
    @see 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
    @see D. M. Henderson, "Euler Angles, Quaternions, and Transformation Matrices",
     JSC 12960, July 1977
    @see Richard E. McFarland, "A Standard Kinematic Model for Flight Simulation at
     NASA-Ames", NASA CR-2497, January 1975
    @see Barnes W. McCormick, "Aerodynamics, Aeronautics, and Flight Mechanics",
     Wiley & Sons, 1979 ISBN 0-471-03032-5
    @see Bernard Etkin, "Dynamics of Flight, Stability and Control", Wiley & Sons,
     1982 ISBN 0-471-08936-2
*/

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

class FGAircraft : public FGModel {
public:
  /** Constructor
      @param Executive a pointer to the parent executive object */
  FGAircraft(FGFDMExec *Executive);

  /// Destructor
  ~FGAircraft();

  /** Runs the Aircraft model; called by the Executive
      @see JSBSim.cpp documentation
      @return false if no error */
  bool Run(void);

  bool InitModel(void);

  /** Loads the aircraft.
      The executive calls this method to load the aircraft into JSBSim.
      @param el a pointer to the element tree
      @return true if successful */
  bool Load(Element* el);

  /** Gets the aircraft name
      @return the name of the aircraft as a string type */
  inline string GetAircraftName(void) { return AircraftName; }

  /// Gets the wing area
  double GetWingArea(void) const { return WingArea; }
  /// Gets the wing span
  double GetWingSpan(void) const { return WingSpan; }
  /// Gets the average wing chord
  double Getcbar(void) const { return cbar; }
  inline double GetWingIncidence(void) const { return WingIncidence; }
  inline double GetWingIncidenceDeg(void) const { return WingIncidence*radtodeg; }
  inline double GetHTailArea(void) const { return HTailArea; }
  inline double GetHTailArm(void)  const { return HTailArm; }
  inline double GetVTailArea(void) const { return VTailArea; }
  inline double GetVTailArm(void)  const { return VTailArm; }
  inline double Getlbarh(void) const { return lbarh; } // HTailArm / cbar
  inline double Getlbarv(void) const { return lbarv; } // VTailArm / cbar
  inline double Getvbarh(void) const { return vbarh; } // H. Tail Volume
  inline double Getvbarv(void) const { return vbarv; } // V. Tail Volume
  inline FGColumnVector3& GetMoments(void) { return vMoments; }
  inline double GetMoments(int idx) const { return vMoments(idx); }
  inline FGColumnVector3& GetForces(void) { return vForces; }
  inline double GetForces(int idx) const { return vForces(idx); }
  inline FGColumnVector3& GetBodyAccel(void) { return vBodyAccel; }
  inline double GetBodyAccel(int idx) { return vBodyAccel(idx); }
  inline FGColumnVector3& GetNcg   (void)  { return vNcg; }
  inline double GetNcg(int idx)  { return vNcg(idx); }
  inline FGColumnVector3& GetXYZrp(void) { return vXYZrp; }
  inline FGColumnVector3& GetXYZvrp(void) { return vXYZvrp; }
  inline FGColumnVector3& GetXYZep(void) { return vXYZep; }
  inline double GetXYZrp(int idx) const { return vXYZrp(idx); }
  inline double GetXYZvrp(int idx) const { return vXYZvrp(idx); }
  inline double GetXYZep(int idx) const { return vXYZep(idx); }
  inline void SetAircraftName(string name) {AircraftName = name;}
  inline void SetHoldDown(int hd) {HoldDown = hd;}
  inline int GetHoldDown(void) const {return HoldDown;}

  void SetXYZrp(int idx, double value) {vXYZrp(idx) = value;}

  void SetWingArea(double S) {WingArea = S;}

  double GetNlf(void);

  inline FGColumnVector3& GetNwcg(void) { return vNwcg; }

  void bind(void);
  void unbind(void);

private:
  FGColumnVector3 vMoments;
  FGColumnVector3 vForces;
  FGColumnVector3 vXYZrp;
  FGColumnVector3 vXYZvrp;
  FGColumnVector3 vXYZep;
  FGColumnVector3 vDXYZcg;
  FGColumnVector3 vBodyAccel;
  FGColumnVector3 vNcg;
  FGColumnVector3 vNwcg;

  double WingArea, WingSpan, cbar, WingIncidence;
  double HTailArea, VTailArea, HTailArm, VTailArm;
  double lbarh,lbarv,vbarh,vbarv;
  int HoldDown;
  string AircraftName;

  void Debug(int from);
};

} // namespace JSBSim
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#endif

