X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FLaRCsim.cxx;h=43223bf4cf9bfbde1f8fc6a0df2a7a126bf3e165;hb=ee98995d30e75cda88c9866f3cb6a761fda7d078;hp=e3134d337517577be630ace1b1da2ced72a54e49;hpb=7cc98ad15f7295cc3665abe6a0d419bf84ada3ac;p=flightgear.git diff --git a/src/FDM/LaRCsim.cxx b/src/FDM/LaRCsim.cxx index e3134d337..43223bf4c 100644 --- a/src/FDM/LaRCsim.cxx +++ b/src/FDM/LaRCsim.cxx @@ -20,12 +20,12 @@ // // $Id$ +#include // strcmp() #include #include -#include - +#include
#include #include #include @@ -33,121 +33,127 @@ #include #include #include +#include #include "IO360.hxx" #include "LaRCsim.hxx" -FGLaRCsim::FGLaRCsim(void) { - ls_toplevel_init( 0.0, (char *)globals->get_options()->get_aircraft().c_str() ); - lsic=new LaRCsimIC; //this needs to be brought up after LaRCsim is - copy_to_LaRCsim(); // initialize all of LaRCsim's vars - //this should go away someday -- formerly done in fg_init.cxx - Mass = 8.547270E+01; - I_xx = 1.048000E+03; - I_yy = 3.000000E+03; - I_zz = 3.530000E+03; - I_xz = 0.000000E+00; - - +FGLaRCsim::FGLaRCsim( double dt ) { +// set_delta_t( dt ); -} + speed_up = fgGetNode("/sim/speed-up", true); + aero = fgGetNode("/sim/aero", true); -FGLaRCsim::~FGLaRCsim(void) { - if(lsic != NULL) { - delete lsic; - } -} + ls_toplevel_init( 0.0, (char *)(aero->getStringValue()) ); -// Initialize the LaRCsim flight model, dt is the time increment for -// each subsequent iteration through the EOM -bool FGLaRCsim::init( double dt ) { - - ls_set_model_dt(dt); - // Initialize our little engine that hopefully might - eng.init(dt); - // dcl - in passing dt to init rather than update I am assuming - // that the LaRCsim dt is fixed at one value (yes it is 120hz CLO) + lsic=new LaRCsimIC; //this needs to be brought up after LaRCsim is + if ( !strcmp(aero->getStringValue(), "c172") ) { + copy_to_LaRCsim(); // initialize all of LaRCsim's vars - // update the engines interface - FGEngInterface e; - add_engine( e ); - - - // FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::init()" ); - - double save_alt = 0.0; - - if ( get_Altitude() < -9000.0 ) { - save_alt = get_Altitude(); - set_Altitude( 0.0 ); + //this should go away someday -- formerly done in fg_init.cxx + Mass = 8.547270E+01; + I_xx = 1.048000E+03; + I_yy = 3.000000E+03; + I_zz = 3.530000E+03; + I_xz = 0.000000E+00; } - // translate FG to LaRCsim structure - copy_to_LaRCsim(); - - // actual LaRCsim top level init - // ls_toplevel_init( dt, (char *)globals->get_options()->get_aircraft().c_str() ); - - - FG_LOG( FG_FLIGHT, FG_INFO, "FG pos = " << - get_Latitude() ); + ls_set_model_dt(dt); - // translate LaRCsim back to FG structure - copy_from_LaRCsim(); + // Initialize our little engine that hopefully might + eng.init(dt); + // dcl - in passing dt to init rather than update I am assuming + // that the LaRCsim dt is fixed at one value (yes it is 120hz CLO) +} - // but lets restore our original bogus altitude when we are done - if ( save_alt < -9000.0 ) { - set_Altitude( save_alt ); +FGLaRCsim::~FGLaRCsim(void) { + if ( lsic != NULL ) { + delete lsic; + lsic = NULL; } +} - // set valid time for this record - stamp_time(); - - return true; +// Initialize the LaRCsim flight model, dt is the time increment for +// each subsequent iteration through the EOM +void FGLaRCsim::init() { + //do init common to all FDM's + common_init(); } // Run an iteration of the EOM (equations of motion) -bool FGLaRCsim::update( int multiloop ) { +void FGLaRCsim::update( double dt ) { - if ( globals->get_options()->get_aircraft() == "c172" ) { + if (is_suspended()) + return; + + int multiloop = _calc_multiloop(dt); + + if ( !strcmp(aero->getStringValue(), "c172") ) { // set control inputs + // cout << "V_calibrated_kts = " << V_calibrated_kts << '\n'; eng.set_IAS( V_calibrated_kts ); - eng.set_Throttle_Lever_Pos( controls.get_throttle( 0 ) * 100.0 ); + eng.set_Throttle_Lever_Pos( globals->get_controls()->get_throttle( 0 ) + * 100.0 ); eng.set_Propeller_Lever_Pos( 100 ); - if ( controls.get_mixture( 0 ) > 0.60 ) { - eng.set_Mixture_Lever_Pos( controls.get_mixture( 0 ) * 100.0 ); - } else { - eng.set_Mixture_Lever_Pos( 60.0 ); - } + eng.set_Mixture_Lever_Pos( globals->get_controls()->get_mixture( 0 ) + * 100.0 ); + eng.set_Magneto_Switch_Pos( globals->get_controls()->get_magnetos(0) ); + eng.setStarterFlag( globals->get_controls()->get_starter(0) ); + eng.set_p_amb( Static_pressure ); + eng.set_T_amb( Static_temperature ); // update engine model eng.update(); + // Fake control-surface positions + fgSetDouble("/surface-positions/flap-pos-norm", + fgGetDouble("/controls/flaps")); + // FIXME: ignoring trim + fgSetDouble("/surface-positions/elevator-pos-norm", + fgGetDouble("/controls/elevator")); + // FIXME: ignoring trim + fgSetDouble("/surface-positions/left-aileron-pos-norm", + fgGetDouble("/controls/aileron")); + // FIXME: ignoring trim + fgSetDouble("/surface-positions/right-aileron-pos-norm", + -1 * fgGetDouble("/controls/aileron")); + // FIXME: ignoring trim + fgSetDouble("/surface-positions/rudder-pos-norm", + fgGetDouble("/controls/rudder")); + // copy engine state values onto "bus" - FGEngInterface *e = get_engine( 0 ); - e->set_Throttle( controls.get_throttle( 0 ) * 100.0 ); - e->set_Mixture( 80 ); - e->set_Prop_Advance( 100 ); - e->set_RPM( eng.get_RPM() ); - e->set_Manifold_Pressure( eng.get_Manifold_Pressure() ); - e->set_MaxHP( eng.get_MaxHP() ); - e->set_Percentage_Power( eng.get_Percentage_Power() ); - e->set_EGT( eng.get_EGT() ); - e->set_prop_thrust( eng.get_prop_thrust_SI() ); - -#if 0 - FG_LOG( FG_FLIGHT, FG_INFO, "Throttle = " << controls.get_throttle( 0 ) * 100.0); - FG_LOG( FG_FLIGHT, FG_INFO, " Mixture = " << 80); - FG_LOG( FG_FLIGHT, FG_INFO, " RPM = " << eng.get_RPM()); - FG_LOG( FG_FLIGHT, FG_INFO, " MP = " << eng.get_Manifold_Pressure()); - FG_LOG( FG_FLIGHT, FG_INFO, " HP = " << ( eng.get_MaxHP() * eng.get_Percentage_Power()/ 100.0) ); - FG_LOG( FG_FLIGHT, FG_INFO, " EGT = " << eng.get_EGT()); - FG_LOG( FG_FLIGHT, FG_INFO, " Thrust (N) " << eng.get_prop_thrust_SI()); // Thrust in Newtons - FG_LOG( FG_FLIGHT, FG_INFO, '\n'); -#endif - // Hmm .. Newtons to lbs is 0.2248 ... - F_X_engine = eng.get_prop_thrust_SI() * 0.07; + fgSetDouble("/engines/engine/rpm", eng.get_RPM()); + fgSetDouble("/engines/engine/mp-osi", eng.get_Manifold_Pressure()); + fgSetDouble("/engines/engine/max-hp", eng.get_MaxHP()); + fgSetDouble("/engines/engine/power-pct", eng.get_Percentage_Power()); + fgSetDouble("/engines/engine/egt-degf", eng.get_EGT()); + fgSetDouble("/engines/engine/cht-degf", eng.get_CHT()); + fgSetDouble("/engines/engine/prop-thrust", eng.get_prop_thrust_SI()); + fgSetDouble("/engines/engine/fuel-flow-gph", + eng.get_fuel_flow_gals_hr()); + fgSetDouble("/engines/engine/oil-temperature-degf", + eng.get_oil_temp()); + fgSetDouble("/engines/engine/running", eng.getRunningFlag()); + fgSetDouble("/engines/engine/cranking", eng.getCrankingFlag()); + + static const SGPropertyNode *fuel_freeze + = fgGetNode("/sim/freeze/fuel"); + + if ( ! fuel_freeze->getBoolValue() ) { + //Assume we are using both tanks equally for now + fgSetDouble("/consumables/fuel/tank[0]/level-gal_us", + fgGetDouble("/consumables/fuel/tank[0]/level-gal_us") + - (eng.get_fuel_flow_gals_hr() / (2 * 3600)) + * dt); + fgSetDouble("/consumables/fuel/tank[1]/level-gal_us", + fgGetDouble("/consumables/fuel/tank[1]/level-gal_us") + - (eng.get_fuel_flow_gals_hr() / (2 * 3600)) + * dt); + } + + F_X_engine = eng.get_prop_thrust_lbs(); + // cout << "F_X_engine = " << F_X_engine << '\n'; } double save_alt = 0.0; @@ -159,33 +165,32 @@ bool FGLaRCsim::update( int multiloop ) { } // copy control positions into the LaRCsim structure - Lat_control = controls.get_aileron() / - globals->get_options()->get_speed_up(); - Long_control = controls.get_elevator(); - Long_trim = controls.get_elevator_trim(); - Rudder_pedal = controls.get_rudder() / - globals->get_options()->get_speed_up(); - Flap_handle = 30.0 * controls.get_flaps(); - - if ( globals->get_options()->get_aircraft() == "c172" ) { - Use_External_Engine = 1; + Lat_control = globals->get_controls()->get_aileron() / + speed_up->getIntValue(); + Long_control = globals->get_controls()->get_elevator(); + Long_trim = globals->get_controls()->get_elevator_trim(); + Rudder_pedal = globals->get_controls()->get_rudder() / + speed_up->getIntValue(); + Flap_handle = 30.0 * globals->get_controls()->get_flaps(); + + if ( !strcmp(aero->getStringValue(), "c172") ) { + Use_External_Engine = 1; } else { Use_External_Engine = 0; } - Throttle_pct = controls.get_throttle( 0 ) * 1.0; + Throttle_pct = globals->get_controls()->get_throttle( 0 ) * 1.0; - Brake_pct[0] = controls.get_brake( 1 ); - Brake_pct[1] = controls.get_brake( 0 ); + Brake_pct[0] = globals->get_controls()->get_brake( 1 ); + Brake_pct[1] = globals->get_controls()->get_brake( 0 ); // Inform LaRCsim of the local terrain altitude // Runway_altitude = get_Runway_altitude(); - Runway_altitude = scenery.cur_elev * METER_TO_FEET; - + Runway_altitude = getACModel()->get3DModel()->getFGLocation()->get_cur_elev_m() * SG_METER_TO_FEET; // Weather /* V_north_airmass = get_V_north_airmass(); - V_east_airmass = get_V_east_airmass(); - V_down_airmass = get_V_down_airmass(); */ + V_east_airmass = get_V_east_airmass(); + V_down_airmass = get_V_down_airmass(); */ // old -- FGInterface_2_LaRCsim() not needed except for Init() @@ -195,16 +200,20 @@ bool FGLaRCsim::update( int multiloop ) { // printf("Altitude = %.2f\n", Altitude * 0.3048); // printf("Radius to Vehicle = %.2f\n", Radius_to_vehicle * 0.3048); - ls_update(multiloop); + // for engine functions (sounds and instruments) + // drive the rpm gauge + fgSetDouble("/engines/engine/rpm", (globals->get_controls()->get_throttle( 0 ) * 100.0 * 25 )); + // manifold air pressure, which drives the sound (see *sound.xml file) + fgSetDouble("/engines/engine/mp-osi", (globals->get_controls()->get_throttle( 0 ) * 100.0 )); + // make the engine cranking and running sounds when fgfs starts up + fgSetDouble("/engines/engine/cranking", 1); + fgSetDouble("/engines/engine/running", 1); - if(isnan(Phi)) { - busdump(); - exit(1); - } + ls_update(multiloop); // printf("%d FG_Altitude = %.2f\n", i, FG_Altitude * 0.3048); // printf("%d Altitude = %.2f\n", i, Altitude * 0.3048); - + // translate LaRCsim back to FG structure so that the // autopilot (and the rest of the sim can use the updated // values @@ -214,8 +223,6 @@ bool FGLaRCsim::update( int multiloop ) { if ( save_alt < -9000.0 ) { set_Altitude( save_alt ); } - - return true; } @@ -430,14 +437,14 @@ bool FGLaRCsim::copy_from_LaRCsim() { _set_Velocities_Local( V_north, V_east, V_down ); // set_Velocities_Ground( V_north_rel_ground, V_east_rel_ground, // V_down_rel_ground ); - // set_Velocities_Local_Airmass( V_north_airmass, V_east_airmass, - // V_down_airmass ); + _set_Velocities_Local_Airmass( V_north_airmass, V_east_airmass, + V_down_airmass ); // set_Velocities_Local_Rel_Airmass( V_north_rel_airmass, // V_east_rel_airmass, V_down_rel_airmass ); // set_Velocities_Gust( U_gust, V_gust, W_gust ); _set_Velocities_Wind_Body( U_body, V_body, W_body ); - // set_V_rel_wind( V_rel_wind ); + _set_V_rel_wind( V_rel_wind ); // set_V_true_kts( V_true_kts ); // set_V_rel_ground( V_rel_ground ); // set_V_inertial( V_inertial ); @@ -450,32 +457,32 @@ bool FGLaRCsim::copy_from_LaRCsim() { _set_Omega_Body( P_body, Q_body, R_body ); // 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_Geocentric_Rates( Latitude_dot, Longitude_dot, Radius_dot ); _set_Mach_number( Mach_number ); - FG_LOG( FG_FLIGHT, FG_DEBUG, "lon = " << Longitude + SG_LOG( SG_FLIGHT, SG_DEBUG, "lon = " << Longitude << " lat_geoc = " << Lat_geocentric << " lat_geod = " << Latitude << " alt = " << Altitude << " sl_radius = " << Sea_level_radius << " radius_to_vehicle = " << Radius_to_vehicle ); double tmp_lon_geoc = Lon_geocentric; - while ( tmp_lon_geoc < -FG_PI ) { tmp_lon_geoc += FG_2PI; } - while ( tmp_lon_geoc > FG_PI ) { tmp_lon_geoc -= FG_2PI; } + while ( tmp_lon_geoc < -SGD_PI ) { tmp_lon_geoc += SGD_2PI; } + while ( tmp_lon_geoc > SGD_PI ) { tmp_lon_geoc -= SGD_2PI; } double tmp_lon = Longitude; - while ( tmp_lon < -FG_PI ) { tmp_lon += FG_2PI; } - while ( tmp_lon > FG_PI ) { tmp_lon -= FG_2PI; } + while ( tmp_lon < -SGD_PI ) { tmp_lon += SGD_2PI; } + while ( tmp_lon > SGD_PI ) { tmp_lon -= SGD_2PI; } // Positions _set_Geocentric_Position( Lat_geocentric, tmp_lon_geoc, - Radius_to_vehicle ); + Radius_to_vehicle ); _set_Geodetic_Position( Latitude, tmp_lon, Altitude ); _set_Euler_Angles( Phi, Theta, Psi ); - _set_Altitude_AGL( Altitude-Runway_altitude ); + _set_Altitude_AGL( Altitude - Runway_altitude ); // Miscellaneous quantities _set_T_Local_to_Body(T_local_to_body_m); @@ -542,165 +549,196 @@ bool FGLaRCsim::copy_from_LaRCsim() { // get_sin_longitude(), get_cos_longitude()); _set_Climb_Rate( -1 * V_down ); + // cout << "climb rate = " << -V_down * 60 << endl; + + if ( !strcmp(aero->getStringValue(), "uiuc") ) { + if (pilot_elev_no) { + globals->get_controls()->set_elevator(Long_control); + globals->get_controls()->set_elevator_trim(Long_trim); + // controls.set_elevator(Long_control); + // controls.set_elevator_trim(Long_trim); + } + if (pilot_ail_no) { + globals->get_controls()->set_aileron(Lat_control); + // controls.set_aileron(Lat_control); + } + if (pilot_rud_no) { + globals->get_controls()->set_rudder(Rudder_pedal); + // controls.set_rudder(Rudder_pedal); + } + if (Throttle_pct_input) { + globals->get_controls()->set_throttle(0,Throttle_pct); + // controls.set_throttle(0,Throttle_pct); + } + } return true; } void FGLaRCsim::set_ls(void) { - Phi=lsic->GetRollAngleRadIC(); - Theta=lsic->GetPitchAngleRadIC(); - Psi=lsic->GetHeadingRadIC(); - V_north=lsic->GetVnorthFpsIC(); - V_east=lsic->GetVeastFpsIC(); - V_down=lsic->GetVdownFpsIC(); - Altitude=lsic->GetAltitudeFtIC(); - Latitude=lsic->GetLatitudeGDRadIC(); - Longitude=lsic->GetLongitudeRadIC(); - Runway_altitude=lsic->GetRunwayAltitudeFtIC(); - V_north_airmass = lsic->GetVnorthAirmassFpsIC(); - V_east_airmass = lsic->GetVeastAirmassFpsIC(); - V_down_airmass = lsic->GetVdownAirmassFpsIC(); - ls_loop(0.0,-1); - copy_from_LaRCsim(); - FG_LOG( FG_FLIGHT, FG_INFO, " FGLaRCsim::set_ls(): " ); - FG_LOG( FG_FLIGHT, FG_INFO, " Phi: " << Phi ); - FG_LOG( FG_FLIGHT, FG_INFO, " Theta: " << Theta ); - FG_LOG( FG_FLIGHT, FG_INFO, " Psi: " << Psi ); - FG_LOG( FG_FLIGHT, FG_INFO, " V_north: " << V_north ); - FG_LOG( FG_FLIGHT, FG_INFO, " V_east: " << V_east ); - FG_LOG( FG_FLIGHT, FG_INFO, " V_down: " << V_down ); - FG_LOG( FG_FLIGHT, FG_INFO, " Altitude: " << Altitude ); - FG_LOG( FG_FLIGHT, FG_INFO, " Latitude: " << Latitude ); - FG_LOG( FG_FLIGHT, FG_INFO, " Longitude: " << Longitude ); - FG_LOG( FG_FLIGHT, FG_INFO, " Runway_altitude: " << Runway_altitude ); - FG_LOG( FG_FLIGHT, FG_INFO, " V_north_airmass: " << V_north_airmass ); - FG_LOG( FG_FLIGHT, FG_INFO, " V_east_airmass: " << V_east_airmass ); - FG_LOG( FG_FLIGHT, FG_INFO, " V_down_airmass: " << V_down_airmass ); -} - - //Positions + Phi=lsic->GetRollAngleRadIC(); + Theta=lsic->GetPitchAngleRadIC(); + Psi=lsic->GetHeadingRadIC(); + V_north=lsic->GetVnorthFpsIC(); + V_east=lsic->GetVeastFpsIC(); + V_down=lsic->GetVdownFpsIC(); + Altitude=lsic->GetAltitudeFtIC(); + Latitude=lsic->GetLatitudeGDRadIC(); + Longitude=lsic->GetLongitudeRadIC(); + Runway_altitude=lsic->GetRunwayAltitudeFtIC(); + V_north_airmass = lsic->GetVnorthAirmassFpsIC() * -1; + V_east_airmass = lsic->GetVeastAirmassFpsIC() * -1; + V_down_airmass = lsic->GetVdownAirmassFpsIC() * -1; + ls_loop(0.0,-1); + copy_from_LaRCsim(); +} + +void FGLaRCsim::snap_shot(void) { + lsic->SetLatitudeGDRadIC( get_Latitude() ); + lsic->SetLongitudeRadIC( get_Longitude() ); + lsic->SetAltitudeFtIC( get_Altitude() ); + lsic->SetRunwayAltitudeFtIC( get_Runway_altitude() ); + lsic->SetVtrueFpsIC( get_V_rel_wind() ); + lsic->SetPitchAngleRadIC( get_Theta() ); + lsic->SetRollAngleRadIC( get_Phi() ); + lsic->SetHeadingRadIC( get_Psi() ); + lsic->SetClimbRateFpsIC( get_Climb_Rate() ); + lsic->SetVNEDAirmassFpsIC( get_V_north_airmass(), + get_V_east_airmass(), + get_V_down_airmass() ); +} + +//Positions void FGLaRCsim::set_Latitude(double lat) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Latitude: " << lat ); - lsic->SetLatitudeGDRadIC(lat); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Latitude: " << lat ); + snap_shot(); + lsic->SetLatitudeGDRadIC(lat); + set_ls(); + copy_from_LaRCsim(); //update the bus +} void FGLaRCsim::set_Longitude(double lon) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Longitude: " << lon ); - lsic->SetLongitudeRadIC(lon); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Longitude: " << lon ); + snap_shot(); + lsic->SetLongitudeRadIC(lon); + set_ls(); + copy_from_LaRCsim(); //update the bus +} void FGLaRCsim::set_Altitude(double alt) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Altitude: " << alt ); - lsic->SetAltitudeFtIC(alt); - set_ls(); - copy_from_LaRCsim(); //update the bus + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Altitude: " << alt ); + snap_shot(); + lsic->SetAltitudeFtIC(alt); + set_ls(); + copy_from_LaRCsim(); //update the bus } - + void FGLaRCsim::set_V_calibrated_kts(double vc) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_V_calibrated_kts: " << vc ); - lsic->SetVcalibratedKtsIC(vc); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, + "FGLaRCsim::set_V_calibrated_kts: " << vc ); + snap_shot(); + lsic->SetVcalibratedKtsIC(vc); + set_ls(); + copy_from_LaRCsim(); //update the bus +} void FGLaRCsim::set_Mach_number(double mach) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Mach_number: " << mach ); - lsic->SetMachIC(mach); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Mach_number: " << mach ); + snap_shot(); + lsic->SetMachIC(mach); + set_ls(); + copy_from_LaRCsim(); //update the bus +} void FGLaRCsim::set_Velocities_Local( double north, double east, double down ){ - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Velocities_local: " - << north << " " << east << " " << down ); - lsic->SetVnorthFpsIC(north); - lsic->SetVeastFpsIC(east); - lsic->SetVdownFpsIC(down); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Velocities_local: " + << north << " " << east << " " << down ); + snap_shot(); + lsic->SetVNEDFpsIC(north, east, down); + set_ls(); + copy_from_LaRCsim(); //update the bus +} void FGLaRCsim::set_Velocities_Wind_Body( double u, double v, double w){ - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Velocities_Wind_Body: " - << u << " " << v << " " << w ); - - lsic->SetUBodyFpsIC(u); - lsic->SetVBodyFpsIC(v); - lsic->SetWBodyFpsIC(w); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Velocities_Wind_Body: " + << u << " " << v << " " << w ); + snap_shot(); + lsic->SetUVWFpsIC(u,v,w); + set_ls(); + copy_from_LaRCsim(); //update the bus +} //Euler angles void FGLaRCsim::set_Euler_Angles( double phi, double theta, double psi ) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Euler_angles: " - << phi << " " << theta << " " << psi ); - - lsic->SetPitchAngleRadIC(theta); - lsic->SetRollAngleRadIC(phi); - lsic->SetHeadingRadIC(psi); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Euler_angles: " + << phi << " " << theta << " " << psi ); + + snap_shot(); + lsic->SetPitchAngleRadIC(theta); + lsic->SetRollAngleRadIC(phi); + lsic->SetHeadingRadIC(psi); + set_ls(); + copy_from_LaRCsim(); //update the bus +} //Flight Path void FGLaRCsim::set_Climb_Rate( double roc) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Climb_rate: " << roc ); - lsic->SetClimbRateFpsIC(roc); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Climb_rate: " << roc ); + snap_shot(); + lsic->SetClimbRateFpsIC(roc); + set_ls(); + copy_from_LaRCsim(); //update the bus +} void FGLaRCsim::set_Gamma_vert_rad( double gamma) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Gamma_vert_rad: " << gamma ); - lsic->SetFlightPathAngleRadIC(gamma); - set_ls(); - copy_from_LaRCsim(); //update the bus -} - -void FGLaRCsim::set_Runway_altitude(double ralt) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Runway_altitude: " << ralt ); - lsic->SetRunwayAltitudeFtIC(ralt); - set_ls(); - copy_from_LaRCsim(); //update the bus -} + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Gamma_vert_rad: " << gamma ); + snap_shot(); + lsic->SetFlightPathAngleRadIC(gamma); + set_ls(); + copy_from_LaRCsim(); //update the bus +} void FGLaRCsim::set_AltitudeAGL(double altagl) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_AltitudeAGL: " << altagl ); - lsic->SetAltitudeAGLFtIC(altagl); - set_ls(); - copy_from_LaRCsim(); + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_AltitudeAGL: " << altagl ); + snap_shot(); + lsic->SetAltitudeAGLFtIC(altagl); + set_ls(); + copy_from_LaRCsim(); } +/* getting a namespace conflict... void FGLaRCsim::set_Velocities_Local_Airmass (double wnorth, - double weast, - double wdown ) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Velocities_Local_Airmass: " - << wnorth << " " << weast << " " << wdown ); - _set_Velocities_Local_Airmass( wnorth, weast, wdown ); - set_ls(); - copy_from_LaRCsim(); -} + double weast, + double wdown ) { + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Velocities_Local_Airmass: " + << wnorth << " " << weast << " " << wdown ); + snap_shot(); + lsic->SetVNEDAirmassFpsIC( wnorth, weast, wdown ); + set_ls(); + copy_from_LaRCsim(); +} +*/ void FGLaRCsim::set_Static_pressure(double p) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Static_pressure: " << p ); - FG_LOG( FG_FLIGHT, FG_INFO, "LaRCsim does not support externally supplied atmospheric data" ); + SG_LOG( SG_FLIGHT, SG_INFO, + "FGLaRCsim::set_Static_pressure: " << p ); + SG_LOG( SG_FLIGHT, SG_INFO, + "LaRCsim does not support externally supplied atmospheric data" ); } void FGLaRCsim::set_Static_temperature(double T) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Static_temperature: " << T ); - FG_LOG( FG_FLIGHT, FG_INFO, "LaRCsim does not support externally supplied atmospheric data" ); + SG_LOG( SG_FLIGHT, SG_INFO, + "FGLaRCsim::set_Static_temperature: " << T ); + SG_LOG( SG_FLIGHT, SG_INFO, + "LaRCsim does not support externally supplied atmospheric data" ); } - -void FGLaRCsim::set_Density(double rho) { - FG_LOG( FG_FLIGHT, FG_INFO, "FGLaRCsim::set_Density: " << rho ); - FG_LOG( FG_FLIGHT, FG_INFO, "LaRCsim does not support externally supplied atmospheric data" ); + +void FGLaRCsim::set_Density(double rho) { + SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Density: " << rho ); + SG_LOG( SG_FLIGHT, SG_INFO, + "LaRCsim does not support externally supplied atmospheric data" ); }