Last rev was based on an old version and blew away recent changes.
Reverted to the current JSBSim CVS version of each.
This commit is contained in:
david
parent
ce69eb8e79
commit
93e0274eb8
2 changed files with 124 additions and 143 deletions
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@ -58,6 +58,12 @@
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#include <FDM/JSBSim/FGPropertyManager.h>
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#include "JSBSim.hxx"
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static inline double
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FMAX (double a, double b)
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{
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return a > b ? a : b;
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}
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/******************************************************************************/
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@ -126,12 +132,12 @@ FGJSBsim::FGJSBsim( double dt )
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init_gear();
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// Set initial fuel levels if provided.
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// Set initial fuel levels if provided.
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for (unsigned int i = 0; i < Propulsion->GetNumTanks(); i++) {
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SGPropertyNode * node = fgGetNode("/consumables/fuel/tank", i, true);
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if (node->getChild("level-gal_us", 0, false) != 0)
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Propulsion->GetTank(i)
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->SetContents(node->getDoubleValue("level-gal_us") * 6.6);
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Propulsion->GetTank(i)
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->SetContents(node->getDoubleValue("level-gal_us") * 6.6);
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}
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fgSetDouble("/fdm/trim/pitch-trim", FCS->GetPitchTrimCmd());
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@ -192,34 +198,9 @@ void FGJSBsim::init() {
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// Explicitly call the superclass's
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// init method first.
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common_init();
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int i;
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ntanks = Propulsion->GetNumTanks();
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tanks = new PROP_NODE_PTR [ntanks];
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for (i = 0; i < ntanks; i++) {
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tanks[i] = fgGetNode("/consumables/fuel/tank", i, true);
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}
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nengines = Propulsion->GetNumEngines();
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engines = new engine_props [nengines];
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for (i = 0; i < nengines; i++) {
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SGPropertyNode *eng = fgGetNode("engines/engine", i);
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engines[i].mp_osi = eng->getNode("mp-osi");
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engines[i].egt_degf = eng->getNode("egt-degf");
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engines[i].fuel_flow_gph = eng->getNode("fuel-flow-gph");
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engines[i].cht_degf = eng->getNode("cht-degf");
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engines[i].oil_temperature_degf = eng->getNode("oil-temperature-degf");
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engines[i].oil_pressure_psi = eng->getNode("oil-pressure-psi");
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engines[i].running = eng->getNode("running");
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engines[i].cranking = eng->getNode("cranking");
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engines[i].rpm = eng->getNode("rpm");
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}
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copy_to_JSBsim();
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fdmex->RunIC(fgic); //loop JSBSim once w/o integrating
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copy_from_JSBsim(); //update the bus
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SG_LOG( SG_FLIGHT, SG_INFO, " Initialized JSBSim with:" );
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@ -284,10 +265,14 @@ FGJSBsim::update( int multiloop ) {
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int i;
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// double save_alt = 0.0;
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copy_to_JSBsim();
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trimmed->setBoolValue(false);
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if ( needTrim ) {
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if ( startup_trim->getBoolValue() ) {
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SG_LOG(SG_FLIGHT, SG_INFO,
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@ -338,31 +323,36 @@ FGJSBsim::update( int multiloop ) {
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bool FGJSBsim::copy_to_JSBsim() {
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unsigned int i;
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// copy control positions into the JSBsim structure
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FGControls *controls = globals->get_controls();
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FCS->SetDaCmd( controls->get_aileron());
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FCS->SetRollTrimCmd( controls->get_aileron_trim() );
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FCS->SetDeCmd( controls->get_elevator());
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FCS->SetPitchTrimCmd( controls->get_elevator_trim() );
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FCS->SetDrCmd( -controls->get_rudder() );
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FCS->SetYawTrimCmd( -controls->get_rudder_trim() );
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FCS->SetDfCmd( controls->get_flaps() );
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FCS->SetDaCmd( globals->get_controls()->get_aileron());
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FCS->SetRollTrimCmd( globals->get_controls()->get_aileron_trim() );
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FCS->SetDeCmd( globals->get_controls()->get_elevator());
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FCS->SetPitchTrimCmd( globals->get_controls()->get_elevator_trim() );
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FCS->SetDrCmd( -globals->get_controls()->get_rudder() );
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FCS->SetYawTrimCmd( -globals->get_controls()->get_rudder_trim() );
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FCS->SetDfCmd( globals->get_controls()->get_flaps() );
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FCS->SetDsbCmd( 0.0 ); //speedbrakes
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FCS->SetDspCmd( 0.0 ); //spoilers
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FCS->SetLBrake( controls->get_brake( 0 ) );
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FCS->SetRBrake( controls->get_brake( 1 ) );
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FCS->SetCBrake( controls->get_brake( 2 ) );
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FCS->SetGearCmd( controls->get_gear_down());
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for (i = 0; i < nengines; i++) {
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// Parking brake sets minimum braking
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// level for mains.
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double parking_brake = globals->get_controls()->get_parking_brake();
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FCS->SetLBrake(FMAX(globals->get_controls()->get_brake(0), parking_brake));
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FCS->SetRBrake(FMAX(globals->get_controls()->get_brake(1), parking_brake));
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FCS->SetCBrake( globals->get_controls()->get_brake( 2 ) );
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FCS->SetGearCmd( globals->get_controls()->get_gear_down());
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for (i = 0; i < Propulsion->GetNumEngines(); i++) {
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FGEngine * eng = Propulsion->GetEngine(i);
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FCS->SetThrottleCmd(i, controls->get_throttle(i));
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FCS->SetMixtureCmd(i, controls->get_mixture(i));
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FCS->SetPropAdvanceCmd(i, controls->get_prop_advance(i));
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Propulsion->GetThruster(i)->SetRPM(engines[i].rpm->getDoubleValue());
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eng->SetMagnetos( controls->get_magnetos(i) );
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eng->SetStarter( controls->get_starter(i) );
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SGPropertyNode * node = fgGetNode("engines/engine", i, true);
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FCS->SetThrottleCmd(i, globals->get_controls()->get_throttle(i));
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FCS->SetMixtureCmd(i, globals->get_controls()->get_mixture(i));
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FCS->SetPropAdvanceCmd(i, globals->get_controls()->get_prop_advance(i));
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Propulsion->GetThruster(i)->SetRPM(node->getDoubleValue("rpm"));
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eng->SetMagnetos( globals->get_controls()->get_magnetos(i) );
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eng->SetStarter( globals->get_controls()->get_starter(i) );
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}
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_set_Runway_altitude( scenery.get_cur_elev() * SG_METER_TO_FEET );
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@ -376,9 +366,16 @@ bool FGJSBsim::copy_to_JSBsim() {
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Atmosphere->SetWindNED(get_V_north_airmass(),
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get_V_east_airmass(),
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get_V_down_airmass());
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// SG_LOG(SG_FLIGHT,SG_INFO, "Wind NED: "
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// << get_V_north_airmass() << ", "
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// << get_V_east_airmass() << ", "
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// << get_V_down_airmass() );
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for (i = 0; i < ntanks; i++) {
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Propulsion->GetTank(i)->SetContents(tanks[i]->getDoubleValue("level-gal_us") * 6.6);
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for (i = 0; i < Propulsion->GetNumTanks(); i++) {
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SGPropertyNode * node = fgGetNode("/consumables/fuel/tank", i, true);
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FGTank * tank = Propulsion->GetTank(i);
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tank->SetContents(node->getDoubleValue("level-gal_us") * 6.6);
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// tank->SetContents(node->getDoubleValue("level-lb"));
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}
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return true;
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@ -459,8 +456,8 @@ bool FGJSBsim::copy_from_JSBsim() {
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// Positions
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_updateGeocentricPosition( Position->GetLatitude(),
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Position->GetLongitude(),
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Position->Geth() );
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Position->GetLongitude(),
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Position->Geth() );
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_set_Altitude_AGL( Position->GetDistanceAGL() );
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@ -486,45 +483,49 @@ bool FGJSBsim::copy_from_JSBsim() {
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}
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}
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// Copy the engine values from JSBSim.
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for( i=0; i < nengines; i++ ) {
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// Copy the engine values from JSBSim.
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for( i=0; i < Propulsion->GetNumEngines(); i++ ) {
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SGPropertyNode * node = fgGetNode("engines/engine", i, true);
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FGEngine * eng = Propulsion->GetEngine(i);
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if(engines[i].mp_osi)
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engines[i].mp_osi->setDoubleValue( eng->getManifoldPressure_inHg());
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if(engines[i].egt_degf)
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engines[i].egt_degf->setDoubleValue( eng->getExhaustGasTemp_degF());
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if(engines[i].fuel_flow_gph)
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engines[i].fuel_flow_gph->setDoubleValue( eng->getFuelFlow_gph());
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if(engines[i].cht_degf)
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engines[i].cht_degf->setDoubleValue( eng->getCylinderHeadTemp_degF());
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if(engines[i].oil_temperature_degf)
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engines[i].oil_temperature_degf->setDoubleValue( eng->getOilTemp_degF());
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if(engines[i].oil_pressure_psi)
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engines[i].oil_pressure_psi->setDoubleValue( eng->getOilPressure_psi());
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if(engines[i].running)
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engines[i].running->setBoolValue( eng->GetRunning());
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if(engines[i].cranking)
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engines[i].cranking->setBoolValue( eng->GetCranking());
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if(engines[i].rpm)
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engines[i].rpm->setDoubleValue( Propulsion->GetThruster(i)->GetRPM());
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FGThruster * thrust = Propulsion->GetThruster(i);
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node->setDoubleValue("mp-osi", eng->getManifoldPressure_inHg());
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node->setDoubleValue("rpm", thrust->GetRPM());
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node->setDoubleValue("egt-degf", eng->getExhaustGasTemp_degF());
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node->setDoubleValue("fuel-flow-gph", eng->getFuelFlow_gph());
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node->setDoubleValue("cht-degf", eng->getCylinderHeadTemp_degF());
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node->setDoubleValue("oil-temperature-degf", eng->getOilTemp_degF());
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node->setDoubleValue("oil-pressure-psi", eng->getOilPressure_psi());
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node->setBoolValue("running", eng->GetRunning());
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node->setBoolValue("cranking", eng->GetCranking());
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}
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static const SGPropertyNode
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*fuel_freeze = fgGetNode("/sim/freeze/fuel");
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static const SGPropertyNode *fuel_freeze
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= fgGetNode("/sim/freeze/fuel");
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// Copy the fuel levels from JSBSim if fuel
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// freeze not enabled.
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// Copy the fuel levels from JSBSim if fuel
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// freeze not enabled.
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if ( ! fuel_freeze->getBoolValue() ) {
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for (i = 0; i < ntanks; i++) {
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double contents = Propulsion->GetTank(i)->GetContents();
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tanks[i]->setDoubleValue("level-gal_us", contents/6.6);
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}
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for (i = 0; i < Propulsion->GetNumTanks(); i++) {
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SGPropertyNode * node
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= fgGetNode("/consumables/fuel/tank", i, true);
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double contents = Propulsion->GetTank(i)->GetContents();
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node->setDoubleValue("level-gal_us", contents/6.6);
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// node->setDoubleValue("level-lb", contents);
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}
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}
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update_gear();
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stall_warning->setDoubleValue( Aircraft->GetStallWarn() );
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/* elevator_pos_deg->setDoubleValue( FCS->GetDePos()*SG_RADIANS_TO_DEGREES );
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left_aileron_pos_deg->setDoubleValue( FCS->GetDaLPos()*SG_RADIANS_TO_DEGREES );
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right_aileron_pos_deg->setDoubleValue( FCS->GetDaRPos()*SG_RADIANS_TO_DEGREES );
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rudder_pos_deg->setDoubleValue( -1*FCS->GetDrPos()*SG_RADIANS_TO_DEGREES );
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flap_pos_deg->setDoubleValue( FCS->GetDfPos() ); */
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elevator_pos_pct->setDoubleValue( FCS->GetDePos(ofNorm) );
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left_aileron_pos_pct->setDoubleValue( FCS->GetDaLPos(ofNorm) );
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right_aileron_pos_pct->setDoubleValue( -1*FCS->GetDaLPos(ofNorm) );
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@ -728,11 +729,11 @@ void FGJSBsim::init_gear(void ) {
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for (int i=0;i<Ngear;i++) {
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SGPropertyNode * node = fgGetNode("gear/gear", i, true);
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node->setDoubleValue("xoffset-in",
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gr->GetGearUnit(i)->GetBodyLocation()(1));
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gr->GetGearUnit(i)->GetBodyLocation()(1));
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node->setDoubleValue("yoffset-in",
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gr->GetGearUnit(i)->GetBodyLocation()(2));
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gr->GetGearUnit(i)->GetBodyLocation()(2));
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node->setDoubleValue("zoffset-in",
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gr->GetGearUnit(i)->GetBodyLocation()(3));
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gr->GetGearUnit(i)->GetBodyLocation()(3));
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node->setBoolValue("wow", gr->GetGearUnit(i)->GetWOW());
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node->setBoolValue("has-brake", gr->GetGearUnit(i)->GetBrakeGroup() > 0);
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node->setDoubleValue("position-norm", FCS->GetGearPos());
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@ -740,24 +741,15 @@ void FGJSBsim::init_gear(void ) {
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}
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void FGJSBsim::update_gear(void) {
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static myNode *nodes;
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static int been_here = 0;
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FGGroundReactions* gr=fdmex->GetGroundReactions();
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int Ngear=GroundReactions->GetNumGearUnits();
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int i;
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if( !been_here ) {
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nodes = new myNode[Ngear];
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for (i=0;i<Ngear;i++) {
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SGPropertyNode * node = fgGetNode("gear/gear", i, true);
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nodes[i][0] = node -> getChild("wow", 0, true);
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nodes[i][1] = node -> getChild("position-norm", 0, true);
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}
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been_here = ~been_here;
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}
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for (i=0;i<Ngear;i++) {
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nodes[i][0] -> setBoolValue(gr->GetGearUnit(i)->GetWOW());
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nodes[i][1] -> setDoubleValue(FCS->GetGearPos());
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for (int i=0;i<Ngear;i++) {
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SGPropertyNode * node = fgGetNode("gear/gear", i, true);
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node->getChild("wow", 0, true)
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->setBoolValue(gr->GetGearUnit(i)->GetWOW());
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node->getChild("position-norm", 0, true)
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->setDoubleValue(FCS->GetGearPos());
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}
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}
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@ -783,14 +775,13 @@ void FGJSBsim::do_trim(void) {
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aileron_trim->setDoubleValue( FCS->GetDaCmd() );
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rudder_trim->setDoubleValue( FCS->GetDrCmd() );
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FGControls *controls = globals->get_controls();
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controls->set_elevator_trim(FCS->GetPitchTrimCmd());
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controls->set_elevator(FCS->GetDeCmd());
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controls->set_throttle(FGControls::ALL_ENGINES,
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FCS->GetThrottleCmd(0));
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globals->get_controls()->set_elevator_trim(FCS->GetPitchTrimCmd());
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globals->get_controls()->set_elevator(FCS->GetDeCmd());
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globals->get_controls()->set_throttle(FGControls::ALL_ENGINES,
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FCS->GetThrottleCmd(0));
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controls->set_aileron(FCS->GetDaCmd());
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controls->set_rudder( FCS->GetDrCmd());
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globals->get_controls()->set_aileron(FCS->GetDaCmd());
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globals->get_controls()->set_rudder( FCS->GetDrCmd());
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SG_LOG( SG_FLIGHT, SG_INFO, " Trim complete" );
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}
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@ -89,6 +89,10 @@ CLASS DOCUMENTATION
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@author Tony Peden (Maintained and refined)
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@version $Id$
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@see main in file JSBSim.cpp (use main() wrapper for standalone usage)
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@see <a href="http://cvs.sourceforge.net/cgi-bin/viewcvs.cgi/jsbsim/JSBSim/JSBSim.hxx?rev=HEAD&content-type=text/vnd.viewcvs-markup">
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Header File </a>
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@see <a href="http://cvs.sourceforge.net/cgi-bin/viewcvs.cgi/jsbsim/JSBSim/JSBSim.cxx?rev=HEAD&content-type=text/vnd.viewcvs-markup">
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Source File </a>
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*/
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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@ -116,17 +120,17 @@ public:
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//@{
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/** Set geocentric latitude
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@param lat latitude in radians measured from the 0 meridian where
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the westerly direction is positive and east is negative */
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the westerly direction is positive and east is negative */
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void set_Latitude(double lat); // geocentric
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/** Set longitude
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@param lon longitude in radians measured from the equator where
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the northerly direction is positive and south is negative */
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the northerly direction is positive and south is negative */
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void set_Longitude(double lon);
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/** Set altitude
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Note: this triggers a recalculation of AGL altitude
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@param alt altitude in feet */
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@param alt altitude in feet */
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void set_Altitude(double alt); // triggers re-calc of AGL altitude
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//@}
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@ -136,33 +140,33 @@ public:
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//@{
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/** Sets calibrated airspeed
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Setting this will trigger a recalc of the other velocity terms.
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@param vc Calibrated airspeed in ft/sec */
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@param vc Calibrated airspeed in ft/sec */
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void set_V_calibrated_kts(double vc);
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/** Sets Mach number.
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Setting this will trigger a recalc of the other velocity terms.
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@param mach Mach number */
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@param mach Mach number */
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void set_Mach_number(double mach);
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/** Sets velocity in N-E-D coordinates.
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Setting this will trigger a recalc of the other velocity terms.
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@param north velocity northward in ft/sec
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@param east velocity eastward in ft/sec
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@param down velocity downward in ft/sec */
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@param north velocity northward in ft/sec
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@param east velocity eastward in ft/sec
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@param down velocity downward in ft/sec */
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void set_Velocities_Local( double north, double east, double down );
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/** Sets aircraft velocity in stability frame.
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Setting this will trigger a recalc of the other velocity terms.
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@param u X velocity in ft/sec
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@param v Y velocity in ft/sec
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@param w Z velocity in ft/sec */
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@param u X velocity in ft/sec
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@param v Y velocity in ft/sec
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@param w Z velocity in ft/sec */
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void set_Velocities_Wind_Body( double u, double v, double w);
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//@}
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||||
|
||||
/** Euler Angle Parameter Set
|
||||
@param phi roll angle in radians
|
||||
@param theta pitch angle in radians
|
||||
@param psi heading angle in radians */
|
||||
@param theta pitch angle in radians
|
||||
@param psi heading angle in radians */
|
||||
void set_Euler_Angles( double phi, double theta, double psi );
|
||||
|
||||
/// @name Flight Path Parameter Set
|
||||
|
|
@ -196,15 +200,15 @@ public:
|
|||
@param weast velocity east in fps
|
||||
@param wdown velocity down in fps*/
|
||||
void set_Velocities_Local_Airmass (double wnorth,
|
||||
double weast,
|
||||
double wdown );
|
||||
double weast,
|
||||
double wdown );
|
||||
/// @name Position Parameter Update
|
||||
//@{
|
||||
|
||||
|
||||
/** Update the position based on inputs, positions, velocities, etc.
|
||||
@param multiloop number of times to loop through the FDM
|
||||
@return true if successful */
|
||||
@return true if successful */
|
||||
void update( int multiloop );
|
||||
bool ToggleDataLogging(bool state);
|
||||
bool ToggleDataLogging(void);
|
||||
|
|
@ -241,6 +245,13 @@ private:
|
|||
SGPropertyNode *rudder_trim;
|
||||
SGPropertyNode *stall_warning;
|
||||
|
||||
/* SGPropertyNode *elevator_pos_deg;
|
||||
SGPropertyNode *left_aileron_pos_deg;
|
||||
SGPropertyNode *right_aileron_pos_deg;
|
||||
SGPropertyNode *rudder_pos_deg;
|
||||
SGPropertyNode *flap_pos_deg; */
|
||||
|
||||
|
||||
SGPropertyNode *elevator_pos_pct;
|
||||
SGPropertyNode *left_aileron_pos_pct;
|
||||
SGPropertyNode *right_aileron_pos_pct;
|
||||
|
|
@ -251,28 +262,7 @@ private:
|
|||
|
||||
void init_gear(void);
|
||||
void update_gear(void);
|
||||
|
||||
// my tweaks start here - NHV
|
||||
typedef SGPropertyNode *PROP_NODE_PTR;
|
||||
typedef PROP_NODE_PTR myNode[2];
|
||||
|
||||
struct engine_props {
|
||||
SGPropertyNode * mp_osi;
|
||||
SGPropertyNode * egt_degf;
|
||||
SGPropertyNode * fuel_flow_gph;
|
||||
SGPropertyNode * cht_degf;
|
||||
SGPropertyNode * oil_temperature_degf;
|
||||
SGPropertyNode * oil_pressure_psi;
|
||||
SGPropertyNode * running;
|
||||
SGPropertyNode * cranking;
|
||||
SGPropertyNode * rpm;
|
||||
} *engines;
|
||||
|
||||
int ntanks;
|
||||
int nengines;
|
||||
|
||||
PROP_NODE_PTR *tanks;
|
||||
|
||||
};
|
||||
|
||||
|
||||
|
|
|
|||
Loading…
Reference in a new issue