Fixed AOA reading on HUD.
Continued work on time jitter compensation.
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529e57a87c
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4 changed files with 71 additions and 12 deletions
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@ -150,7 +150,7 @@ double get_aoa( void )
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FGState *f;
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f = current_aircraft.fdm_state;
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return( f->get_Gamma_vert_rad() * RAD_TO_DEG );
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return( f->get_Alpha() * RAD_TO_DEG );
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}
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double get_roll( void )
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@ -303,6 +303,10 @@ void fgCockpitUpdate( void ) {
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// $Log$
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// Revision 1.29 1999/01/08 19:27:34 curt
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// Fixed AOA reading on HUD.
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// Continued work on time jitter compensation.
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//
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// Revision 1.28 1999/01/07 20:24:17 curt
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// Update fgGENERAL to FGGeneral.
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//
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@ -322,7 +322,7 @@ int fgLaRCsim_2_FGState (FGState& f) {
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// f.set_Omega_Total( P_total, Q_total, R_total );
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// f.set_Euler_Rates( Phi_dot, Theta_dot, Psi_dot );
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// f.set_Geocentric_Rates( Latitude_dot, Longitude_dot, Radius_dot );
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f.set_Geocentric_Rates( Latitude_dot, Longitude_dot, Radius_dot );
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// Positions
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f.set_Geocentric_Position( Lat_geocentric, Lon_geocentric,
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@ -335,7 +335,7 @@ int fgLaRCsim_2_FGState (FGState& f) {
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// f.set_Gravity( Gravity );
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// f.set_Centrifugal_relief( Centrifugal_relief );
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// f.set_Alpha( Alpha );
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f.set_Alpha( Alpha );
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f.set_Beta( Beta );
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// f.set_Alpha_dot( Alpha_dot );
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// f.set_Beta_dot( Beta_dot );
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@ -389,6 +389,10 @@ int fgLaRCsim_2_FGState (FGState& f) {
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// $Log$
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// Revision 1.9 1999/01/08 19:27:36 curt
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// Fixed AOA reading on HUD.
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// Continued work on time jitter compensation.
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//
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// Revision 1.8 1998/12/18 23:37:06 curt
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// Collapsed out the FGState variables not currently needed. They are just
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// commented out and can be readded easily at any time. The point of this
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@ -90,6 +90,43 @@ int fgFlightModelInit(int model, FGState& f, double dt) {
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}
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// Extrapolate fdm based on jitter time (in milliseconds)
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static FGState extrapolate_fdm( FGState &base, int jitter ) {
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FGState result;
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double dt = jitter / 1000.0;
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// cout << "dt = " << dt << endl;
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// start by making a straight up copy
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result = base;
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double lon = base.get_Longitude() + base.get_Longitude_dot() * dt;
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double lon_geoc = base.get_Lon_geocentric() + base.get_Longitude_dot() * dt;
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double lat = base.get_Latitude() + base.get_Latitude_dot() * dt;
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double lat_geoc = base.get_Lat_geocentric() + base.get_Latitude_dot() * dt;
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/*
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cout << "( " << base.get_Longitude() << ", " <<
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base.get_Latitude() << " )" << endl;
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cout << "( " << lon << ", " << lat << " )" << endl;
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cout << "( " << base.get_Longitude_dot() * dt << ", " <<
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base.get_Latitude_dot() * dt << ", " <<
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base.get_Radius_dot() * dt << " )" << endl;
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*/
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double alt = base.get_Altitude() + base.get_Radius_dot() * dt;
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double radius = base.get_Radius_to_vehicle() + base.get_Radius_dot() * dt;
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result.set_Longitude( lon );
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result.set_Latitude( lat );
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result.set_Altitude( alt );
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// result.set_Geocentric_Position( lon_geoc, lat_geoc, radius );
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return result;
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}
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// Run multiloop iterations of the flight model
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int fgFlightModelUpdate(int model, FGState& f, int multiloop, int jitter) {
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double time_step, start_elev, end_elev;
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@ -119,7 +156,7 @@ int fgFlightModelUpdate(int model, FGState& f, int multiloop, int jitter) {
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base_fdm_state.set_Climb_Rate( (end_elev - start_elev) / time_step );
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}
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f = base_fdm_state;
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f = extrapolate_fdm( base_fdm_state, jitter );
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return 1;
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}
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@ -147,6 +184,10 @@ void fgFlightModelSetAltitude(int model, double alt_meters) {
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// $Log$
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// Revision 1.9 1999/01/08 19:27:37 curt
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// Fixed AOA reading on HUD.
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// Continued work on time jitter compensation.
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//
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// Revision 1.8 1999/01/08 03:23:51 curt
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// Beginning work on compensating for sim time vs. real world time "jitter".
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//
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@ -52,6 +52,7 @@
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`FGState::get_Gamma_vert_rad ()'
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`FGState::get_Climb_Rate ()'
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`FGState::get_Alpha ()'
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`FGState::get_Beta ()'
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`FGState::get_Runway_altitude ()'
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@ -61,6 +62,10 @@
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`FGState::get_Sea_level_radius ()'
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`FGState::get_Earth_position_angle ()'
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`FGState::get_Latitude_dot()'
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`FGState::get_Longitude_dot()'
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`FGState::get_Radius_dot()'
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`FGState::get_Dx_cg ()'
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`FGState::get_Dy_cg ()'
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`FGState::get_Dz_cg ()'
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@ -511,14 +516,14 @@ public:
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FG_VECTOR_3 geocentric_rates_v; // Geocentric linear velocities
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// inline double * get_Geocentric_rates_v() { return geocentric_rates_v; }
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// inline double get_Latitude_dot() const { return geocentric_rates_v[0]; }
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// inline double get_Longitude_dot() const { return geocentric_rates_v[1]; }
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// inline double get_Radius_dot() const { return geocentric_rates_v[2]; }
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/* inline void set_Geocentric_Rates( double lat, double lon, double rad ) {
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inline double get_Latitude_dot() const { return geocentric_rates_v[0]; }
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inline double get_Longitude_dot() const { return geocentric_rates_v[1]; }
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inline double get_Radius_dot() const { return geocentric_rates_v[2]; }
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inline void set_Geocentric_Rates( double lat, double lon, double rad ) {
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geocentric_rates_v[0] = lat;
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geocentric_rates_v[1] = lon;
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geocentric_rates_v[2] = rad;
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} */
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}
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/*=============================== Positions ===============================*/
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@ -538,7 +543,8 @@ public:
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inline void set_Radius_to_vehicle(double radius) {
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geocentric_position_v[2] = radius;
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}
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inline void set_Geocentric_Position( double lat, double lon, double rad ) {
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// inline void set_Geocentric_Position( double lat, double lon, double rad ) {
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geocentric_position_v[0] = lat;
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geocentric_position_v[1] = lon;
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geocentric_position_v[2] = rad;
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@ -621,8 +627,8 @@ public:
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// inline void set_Centrifugal_relief(double cr) { centrifugal_relief = cr; }
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double alpha, beta, alpha_dot, beta_dot; // in radians
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// inline double get_Alpha() const { return alpha; }
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// inline void set_Alpha( double a ) { alpha = a; }
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inline double get_Alpha() const { return alpha; }
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inline void set_Alpha( double a ) { alpha = a; }
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inline double get_Beta() const { return beta; }
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inline void set_Beta( double b ) { beta = b; }
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// inline double get_Alpha_dot() const { return alpha_dot; }
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@ -791,6 +797,10 @@ void fgFlightModelSetAltitude(int model, double alt_meters);
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// $Log$
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// Revision 1.9 1999/01/08 19:27:38 curt
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// Fixed AOA reading on HUD.
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// Continued work on time jitter compensation.
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//
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// Revision 1.8 1999/01/08 03:23:52 curt
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// Beginning work on compensating for sim time vs. real world time "jitter".
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//
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