-/*******************************************************************************
-
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
Header: FGAtmosphere.h
Author: Jon Berndt
Implementation of 1959 Standard Atmosphere added by Tony Peden
Date started: 11/24/98
-
+
------------- 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
--------------------------------------------------------------------------------
11/24/98 JSB Created
-07/23/99 TP Added implementation of 1959 Standard Atmosphere
- Moved calculation of Mach number to FGTranslation
-
-
-********************************************************************************
+07/23/99 TP Added implementation of 1959 Standard Atmosphere
+ Moved calculation of Mach number to FGPropagate
+ Updated to '76 model
+
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
SENTRY
-*******************************************************************************/
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#ifndef FGAtmosphere_H
#define FGAtmosphere_H
-/*******************************************************************************
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
INCLUDES
-*******************************************************************************/
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#include "FGModel.h"
+#include "FGColumnVector3.h"
-/*******************************************************************************
-COMMENTS, REFERENCES, and NOTES
-********************************************************************************
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+DEFINITIONS
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
-[1] Anderson, John D. "Introduction to Flight, Third Edition", McGraw-Hill,
- 1989, ISBN 0-07-001641-0
+#define ID_ATMOSPHERE "$Id$"
-/*******************************************************************************
-CLASS DECLARATION
-*******************************************************************************/
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+FORWARD DECLARATIONS
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
+
+namespace JSBSim {
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+CLASS DOCUMENTATION
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
-using namespace std;
+/** Models the standard atmosphere.
+ @author Tony Peden, Jon Berndt
+ @version $Id$
+ @see Anderson, John D. "Introduction to Flight, Third Edition", McGraw-Hill,
+ 1989, ISBN 0-07-001641-0
+*/
-class FGAtmosphere : public FGModel
-{
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+CLASS DECLARATION
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
+
+class FGAtmosphere : public FGModel {
public:
+ /// Constructor
FGAtmosphere(FGFDMExec*);
- ~FGAtmosphere(void);
+ /// Destructor
+ ~FGAtmosphere();
+ /** Runs the Atmosphere model; called by the Executive
+ @return false if no error */
bool Run(void);
- inline float Getrho(void) {return rho;}
- float CalcRho(float altitude);
-
- inline float GetTemperature(void){return temperature;}
- inline float GetDensity(void) {return density;} // use only after Run() has been called
- inline float GetPressure(void) {return pressure;}
- inline float GetSoundSpeed(void) {return soundspeed;}
-
- float GetTemperature(float altitude); //Rankine, altitude in feet
- float GetDensity(float altitude); //slugs/ft^3
- float GetPressure(float altitude); //lbs/ft^2
- float GetSoundSpeed(float altitude); //ft/s
-
+ bool InitModel(void);
+
+ /// Returns the temperature in degrees Rankine.
+ inline double GetTemperature(void) const {return *temperature;}
+ /** Returns the density in slugs/ft^3.
+ <i>This function may <b>only</b> be used if Run() is called first.</i> */
+ inline double GetDensity(void) const {return *density;}
+ /// Returns the pressure in psf.
+ inline double GetPressure(void) const {return *pressure;}
+ /// Returns the pressure at an arbitrary altitude in psf
+ double GetPressure(double alt);
+ /// Returns the speed of sound in ft/sec.
+ inline double GetSoundSpeed(void) const {return soundspeed;}
+
+ /// Returns the sea level temperature in degrees Rankine.
+ inline double GetTemperatureSL(void) const { return SLtemperature; }
+ /// Returns the sea level density in slugs/ft^3
+ inline double GetDensitySL(void) const { return SLdensity; }
+ /// Returns the sea level pressure in psf.
+ inline double GetPressureSL(void) const { return SLpressure; }
+ /// Returns the sea level speed of sound in ft/sec.
+ inline double GetSoundSpeedSL(void) const { return SLsoundspeed; }
+
+ /// Returns the ratio of at-altitude temperature over the sea level value.
+ inline double GetTemperatureRatio(void) const { return (*temperature)*rSLtemperature; }
+ /// Returns the ratio of at-altitude density over the sea level value.
+ inline double GetDensityRatio(void) const { return (*density)*rSLdensity; }
+ /// Returns the ratio of at-altitude pressure over the sea level value.
+ inline double GetPressureRatio(void) const { return (*pressure)*rSLpressure; }
+ /// Returns the ratio of at-altitude sound speed over the sea level value.
+ inline double GetSoundSpeedRatio(void) const { return soundspeed*rSLsoundspeed; }
+
+ /// Tells the simulator to use an externally calculated atmosphere model.
+ void UseExternal(void);
+ /// Tells the simulator to use the internal atmosphere model.
+ void UseInternal(void); //this is the default
+ /// Gets the boolean that tells if the external atmosphere model is being used.
+ bool External(void) { return useExternal; }
+
+ /// Provides the external atmosphere model with an interface to set the temperature.
+ inline void SetExTemperature(double t) { exTemperature=t; }
+ /// Provides the external atmosphere model with an interface to set the density.
+ inline void SetExDensity(double d) { exDensity=d; }
+ /// Provides the external atmosphere model with an interface to set the pressure.
+ inline void SetExPressure(double p) { exPressure=p; }
+
+ /// Sets the temperature deviation at sea-level in degrees Fahrenheit
+ inline void SetSLTempDev(double d) { T_dev_sl = d; }
+ /// Gets the temperature deviation at sea-level in degrees Fahrenheit
+ inline double GetSLTempDev(void) const { return T_dev_sl; }
+ /// Sets the current delta-T in degrees Fahrenheit
+ inline void SetDeltaT(double d) { delta_T = d; }
+ /// Gets the current delta-T in degrees Fahrenheit
+ inline double GetDeltaT(void) const { return delta_T; }
+ /// Gets the at-altitude temperature deviation in degrees Fahrenheit
+ inline double GetTempDev(void) const { return T_dev; }
+ /// Gets the density altitude in feet
+ inline double GetDensityAltitude(void) const { return density_altitude; }
+
+ /// Sets the wind components in NED frame.
+ inline void SetWindNED(double wN, double wE, double wD) { vWindNED(1)=wN; vWindNED(2)=wE; vWindNED(3)=wD;}
+
+ /// Retrieves the wind components in NED frame.
+ inline FGColumnVector3& GetWindNED(void) { return vWindNED; }
+
+ /** Retrieves the wind direction. The direction is defined as north=0 and
+ increases counterclockwise. The wind heading is returned in radians.*/
+ inline double GetWindPsi(void) const { return psiw; }
+
+ inline void SetTurbGain(double tt) {TurbGain = tt;}
+ inline void SetTurbRate(double tt) {TurbRate = tt;}
+
+ inline double GetTurbPQR(int idx) const {return vTurbPQR(idx);}
+ inline FGColumnVector3& GetTurbPQR(void) {return vTurbPQR;}
+
+ void bind(void);
+ void unbind(void);
+
+
protected:
-
-private:
- float rho;
-
- float h;
- float temperature;
- float pressure;
- float density;
- float soundspeed;
- void Calculate(void);
-
-
+ double rho;
+
+ enum tType {ttStandard, ttBerndt, ttNone} turbType;
+
+ int lastIndex;
+ double h;
+ double htab[8];
+ double SLtemperature,SLdensity,SLpressure,SLsoundspeed;
+ double rSLtemperature,rSLdensity,rSLpressure,rSLsoundspeed; //reciprocals
+ double *temperature,*density,*pressure;
+ double soundspeed;
+ bool useExternal;
+ double exTemperature,exDensity,exPressure;
+ double intTemperature, intDensity, intPressure;
+ double T_dev_sl, T_dev, delta_T, density_altitude;
+
+ double MagnitudedAccelDt, MagnitudeAccel, Magnitude;
+ double TurbGain;
+ double TurbRate;
+ FGColumnVector3 vDirectiondAccelDt;
+ FGColumnVector3 vDirectionAccel;
+ FGColumnVector3 vDirection;
+ FGColumnVector3 vTurbulence;
+ FGColumnVector3 vTurbulenceGrad;
+ FGColumnVector3 vBodyTurbGrad;
+ FGColumnVector3 vTurbPQR;
+
+ FGColumnVector3 vWindNED;
+ double psiw;
+
+ void Calculate(double altitude);
+ void Turbulence(void);
+ void Debug(int from);
};
-/******************************************************************************/
+} // namespace JSBSim
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#endif
+
projects / flightgear.git / blobdiff