Updates so that JSBsim can work.
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a1b2152d7f
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3 changed files with 24 additions and 4 deletions
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@ -54,7 +54,7 @@ FGFDMExec FDMExec;
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// Initialize the JSBsim flight model, dt is the time increment for
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// each subsequent iteration through the EOM
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int fgJSBsimInit(double dt) {
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int fgJSBsimInit(double dt, FGInterface& f) {
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FG_LOG( FG_FLIGHT, FG_INFO, "Starting initializing JSBsim" );
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FG_LOG( FG_FLIGHT, FG_INFO, " created FDMExec" );
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@ -69,7 +69,27 @@ int fgJSBsimInit(double dt) {
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engine_path.str(), "X15");
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FG_LOG( FG_FLIGHT, FG_INFO, " loaded aircraft" );
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FDMExec.GetState()->Reset(aircraft_path.str(), "Reset00");
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// FDMExec.GetState()->Reset(aircraft_path.str(), "Reset00");
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FDMExec.GetState()->Initialize(
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current_options.get_uBody(),
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current_options.get_vBody(),
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current_options.get_wBody(),
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f.get_Phi(),
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f.get_Theta(),
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f.get_Psi(),
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f.get_Latitude() * RAD_TO_DEG,
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f.get_Longitude() * RAD_TO_DEG,
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f.get_Altitude()
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);
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// FDMExec.GetState()->Setlatitude(f.get_Latitude());
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// FDMExec.GetState()->Setlongitude(f.get_Longitude());
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// FDMExec.GetState()->Seth(f.get_Altitude());
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// FDMExec.GetRotation()->Setphi(f.get_Phi());
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// FDMExec.GetRotation()->Settht(f.get_Theta());
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// FDMExec.GetRotation()->Setpsi(f.get_Psi());
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FG_LOG( FG_FLIGHT, FG_INFO, " loaded initial conditions" );
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FDMExec.GetState()->Setdt(dt);
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@ -31,7 +31,7 @@
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// reset flight params to a specific position
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int fgJSBsimInit(double dt);
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int fgJSBsimInit(double dt, FGInterface& f);
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// update position based on inputs, positions, velocities, etc.
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int fgJSBsimUpdate(FGInterface& f, int multiloop);
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@ -86,7 +86,7 @@ int fgFDMInit(int model, FGInterface& f, double dt) {
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// fgSlewInit(dt);
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#ifndef __MWERKS__ // -dw- 04/22/99 JSB sim not ported yet
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} else if ( model == FGInterface::FG_JSBSIM ) {
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fgJSBsimInit(dt);
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fgJSBsimInit(dt, f);
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fgJSBsim_2_FGInterface(base_fdm_state);
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#endif
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} else if ( model == FGInterface::FG_LARCSIM ) {
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