2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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2000-10-02 23:07:30 +00:00
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Header: FGAerodynamics.h
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Author: Jon S. Berndt
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Date started: 09/13/00
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------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------
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This program is free software; you can redistribute it and/or modify it under
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the terms of the GNU General Public License as published by the Free Software
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Foundation; either version 2 of the License, or (at your option) any later
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version.
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This program is distributed in the hope that it will be useful, but WITHOUT
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ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
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FOR A PARTICULAR PURPOSE. See the GNU General Public License for more
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details.
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You should have received a copy of the GNU General Public License along with
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this program; if not, write to the Free Software Foundation, Inc., 59 Temple
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Place - Suite 330, Boston, MA 02111-1307, USA.
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Further information about the GNU General Public License can also be found on
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the world wide web at http://www.gnu.org.
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HISTORY
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--------------------------------------------------------------------------------
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09/13/00 JSB Created
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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2000-10-02 23:07:30 +00:00
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SENTRY
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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2000-10-02 23:07:30 +00:00
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#ifndef FGAERODYNAMICS_H
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#define FGAERODYNAMICS_H
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2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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2000-10-02 23:07:30 +00:00
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INCLUDES
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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2000-10-02 23:07:30 +00:00
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#ifdef FGFS
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# include <simgear/compiler.h>
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2001-03-23 22:15:19 +00:00
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# ifdef SG_HAVE_STD_INCLUDES
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# include <vector>
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# else
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# include <vector.h>
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# endif
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#else
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# include <vector>
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#endif
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#include "FGModel.h"
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#include "FGConfigFile.h"
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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DEFINITIONS
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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2000-10-14 02:10:10 +00:00
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#define ID_AERODYNAMICS "$Header$"
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2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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FORWARD DECLARATIONS
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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COMMENTS, REFERENCES, and NOTES [use "class documentation" below for API docs]
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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CLASS DOCUMENTATION
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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/** Encapsulates the aerodynamic calculations.
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This class owns and contains the list of coefficients that define the
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aerodynamic properties of this aircraft. Here also, such unique phenomena
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as ground effect and maximum lift curve tailoff are handled.
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@author Jon S. Berndt
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@version $Id$
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@see -
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*/
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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CLASS DECLARATION
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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class FGAerodynamics : public FGModel {
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public:
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/** Constructor
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@param Executive a pointer to the parent executive object */
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FGAerodynamics(FGFDMExec*);
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/// Destructor
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~FGAerodynamics(void);
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/** Runs the Aerodynamics model; called by the Executive
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@return false if no error */
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bool Run(void);
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/** Loads the Aerodynamics model
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@return true if successful */
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bool LoadAerodynamics(FGConfigFile* AC_cfg);
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};
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2000-11-03 23:02:47 +00:00
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//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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#endif
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