Author: Jon Berndt
Date started: 01/26/99
- ------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------
+ ------------- Copyright (C) 1999 Jon S. Berndt (jon@jsbsim.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
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#include "FGModel.h"
-#include <math/FGColumnVector3.h>
-#include <math/FGLocation.h>
+#include "math/FGColumnVector3.h"
+#include "math/FGLocation.h"
#include "FGPropagate.h"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
/// Destructor
~FGAuxiliary();
+ bool InitModel(void);
+
/** Runs the Auxiliary routines; called by the Executive
@return false if no error */
bool Run(void);
// GET functions
// Atmospheric parameters GET functions
+ /** Returns Calibrated airspeed in feet/second.*/
double GetVcalibratedFPS(void) const { return vcas; }
+ /** Returns Calibrated airspeed in knots.*/
double GetVcalibratedKTS(void) const { return vcas*fpstokts; }
+ /** Returns equivalent airspeed in feet/second. */
double GetVequivalentFPS(void) const { return veas; }
+ /** Returns equivalent airspeed in knots. */
double GetVequivalentKTS(void) const { return veas*fpstokts; }
- // total pressure above is freestream total pressure for subsonic only
- // for supersonic it is the 1D total pressure behind a normal shock
+ /** Returns the total pressure.
+ Total pressure is freestream total pressure for
+ subsonic only. For supersonic it is the 1D total pressure
+ behind a normal shock. */
double GetTotalPressure(void) const { return pt; }
+
+ /** Returns the total temperature.
+ The total temperature ("tat", isentropic flow) is calculated:
+ @code
+ tat = sat*(1 + 0.2*Mach*Mach)
+ @endcode
+ (where "sat" is standard temperature) */
+
double GetTotalTemperature(void) const { return tat; }
double GetTAT_C(void) const { return tatc; }
double GetMagBeta (void) const { return fabs(beta); }
double Getalpha (int unit) const { if (unit == inDegrees) return alpha*radtodeg;
- else cerr << "Bad units" << endl; return 0.0;}
+ else return BadUnits(); }
double Getbeta (int unit) const { if (unit == inDegrees) return beta*radtodeg;
- else cerr << "Bad units" << endl; return 0.0;}
+ else return BadUnits(); }
double Getadot (int unit) const { if (unit == inDegrees) return adot*radtodeg;
- else cerr << "Bad units" << endl; return 0.0;}
+ else return BadUnits(); }
double Getbdot (int unit) const { if (unit == inDegrees) return bdot*radtodeg;
- else cerr << "Bad units" << endl; return 0.0;}
+ else return BadUnits(); }
double GetMagBeta (int unit) const { if (unit == inDegrees) return fabs(beta)*radtodeg;
- else cerr << "Bad units" << endl; return 0.0;}
+ else return BadUnits(); }
+
+ double Getqbar (void) const { return qbar; }
+ double GetqbarUW (void) const { return qbarUW; }
+ double GetqbarUV (void) const { return qbarUV; }
+ double GetReynoldsNumber(void) const { return Re; }
+
+ /** Gets the magnitude of total vehicle velocity including wind effects in feet per second. */
+ double GetVt (void) const { return Vt; }
+
+ /** Gets the ground speed in feet per second.
+ The magnitude is the square root of the sum of the squares (RSS) of the
+ vehicle north and east velocity components.
+ @return The magnitude of the vehicle velocity in the horizontal plane. */
+ double GetVground (void) const { return Vground; }
+
+ /** Gets the Mach number. */
+ double GetMach (void) const { return Mach; }
- double Getqbar (void) const { return qbar; }
- double GetqbarUW (void) const { return qbarUW; }
- double GetqbarUV (void) const { return qbarUV; }
- double GetVt (void) const { return Vt; }
- double GetVground (void) const { return Vground; }
- double GetMach (void) const { return Mach; }
- double GetMachU (void) const { return MachU; }
+ /** The mach number calculated using the vehicle X axis velocity. */
+ double GetMachU (void) const { return MachU; }
+
+ /** The vertical acceleration in g's of the aircraft center of gravity. */
+ double GetNz (void) const { return Nz; }
double GetHOverBCG(void) const { return hoverbcg; }
double GetHOverBMAC(void) const { return hoverbmac; }
double GetGamma(void) const { return gamma; }
double GetGroundTrack(void) const { return psigt; }
- double GetEarthPositionAngle(void) const { return earthPosAngle; }
- double GetHeadWind(void);
- double GetCrossWind(void);
+ double GetHeadWind(void) const;
+ double GetCrossWind(void) const;
// SET functions
void SetAB (double t1, double t2) { alpha=t1; beta=t2; }
void SetGamma (double tt) { gamma = tt; }
-// Time routines, SET and GET functions
+// Time routines, SET and GET functions, used by FGMSIS atmosphere
void SetDayOfYear (int doy) { day_of_year = doy; }
void SetSecondsInDay (double sid) { seconds_in_day = sid; }
int GetDayOfYear (void) const { return day_of_year; }
double GetSecondsInDay (void) const { return seconds_in_day; }
- void bind(void);
- void unbind(void);
+ double GetLongitudeRelativePosition (void) const { return lon_relative_position; }
+ double GetLatitudeRelativePosition (void) const { return lat_relative_position; }
+ double GetDistanceRelativePosition (void) const { return relative_position; }
+
+ void SetAeroPQR(FGColumnVector3 tt) { vAeroPQR = tt; }
private:
double vcas, veas;
FGColumnVector3 vEuler;
FGColumnVector3 vEulerRates;
FGColumnVector3 vMachUVW;
+ FGColumnVector3 vAircraftAccel;
FGLocation vLocationVRP;
double Vt, Vground, Mach, MachU;
double qbar, qbarUW, qbarUV;
+ double Re; // Reynolds Number = V*c/mu
double alpha, beta;
double adot,bdot;
double psigt, gamma;
+ double Nz;
double seconds_in_day; // seconds since current GMT day began
int day_of_year; // GMT day, 1 .. 366
- double earthPosAngle;
double hoverbcg, hoverbmac;
+ // helper data, calculation of distance from initial position
+
+ double lon_relative_position;
+ double lat_relative_position;
+ double relative_position;
+
+ void CalculateRelativePosition(void);
+
+ void bind(void);
+ double BadUnits(void) const;
void Debug(int from);
};
projects / flightgear.git / blobdiff