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Changes by Tony Peden to get pitch, roll, and yaw rates onto the "bus."

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curt 2000-04-11 21:45:42 +00:00
parent a0ed3977ce
commit 12168687cb
5 changed files with 8 additions and 5 deletions
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2
src/FDM/Balloon.cxx
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@ -198,7 +198,7 @@ int FGBalloonSim::copy_from_BalloonSim() {
current_balloon.getHPR( temp );
set_Euler_Angles( temp[0], temp[1], temp[2] );
set_Euler_Rates(0,0,0);
set_Alpha( 0.0/*FDMExec.GetTranslation()->Getalpha()*/ );
set_Beta( 0.0/*FDMExec.GetTranslation()->Getbeta()*/ );

4
src/FDM/JSBSim.cxx
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@ -209,7 +209,9 @@ int FGJSBsim::copy_from_JSBsim() {
// set_Omega_Local( P_local, Q_local, R_local );
// set_Omega_Total( P_total, Q_total, R_total );
// set_Euler_Rates( Phi_dot, Theta_dot, Psi_dot );
set_Euler_Rates( FDMExec.GetRotation()->Getphi(),
FDMExec.GetRotation()->Gettht(),
FDMExec.GetRotation()->Getpsi() );
// ***FIXME*** set_Geocentric_Rates( Latitude_dot, Longitude_dot, Radius_dot );
set_Mach_number( FDMExec.GetState()->GetMach());

2
src/FDM/LaRCsim.cxx
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@ -360,7 +360,7 @@ int FGLaRCsim::copy_from_LaRCsim() {
// set_Omega_Local( P_local, Q_local, R_local );
// set_Omega_Total( P_total, Q_total, R_total );
// set_Euler_Rates( Phi_dot, Theta_dot, Psi_dot );
set_Euler_Rates( Phi_dot, Theta_dot, Psi_dot );
set_Geocentric_Rates( Latitude_dot, Longitude_dot, Radius_dot );
set_Mach_number( mach_number );

1
src/FDM/MagicCarpet.cxx
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@ -62,6 +62,7 @@ int FGMagicCarpet::update( int multiloop ) {
// update euler angles
set_Euler_Angles( get_Phi(), get_Theta(), fmod(get_Psi() + turn, FG_2PI) );
set_Euler_Rates(0,0,0);
// update (lon/lat) position
double lat2, lon2, az2;

4
src/FDM/flight.hxx
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@ -532,11 +532,11 @@ public:
// inline double get_Phi_dot() const { return euler_rates_v[0]; }
// inline double get_Theta_dot() const { return euler_rates_v[1]; }
// inline double get_Psi_dot() const { return euler_rates_v[2]; }
/* inline void set_Euler_Rates( double phi, double theta, double psi ) {
inline void set_Euler_Rates( double phi, double theta, double psi ) {
euler_rates_v[0] = phi;
euler_rates_v[1] = theta;
euler_rates_v[2] = psi;
} */
}
FG_VECTOR_3 geocentric_rates_v; // Geocentric linear velocities
// inline double * get_Geocentric_rates_v() { return geocentric_rates_v; }