#endif
#include <simgear/compiler.h>
+#include <simgear/sg_inlines.h>
#include <stdio.h> // size_t
#include <string>
#include <FDM/JSBSim/models/FGLGear.h>
#include <FDM/JSBSim/models/FGGroundReactions.h>
#include <FDM/JSBSim/models/FGPropulsion.h>
+#include <FDM/JSBSim/models/FGAccelerations.h>
+#include <FDM/JSBSim/models/atmosphere/FGWinds.h>
#include <FDM/JSBSim/models/propulsion/FGEngine.h>
#include <FDM/JSBSim/models/propulsion/FGPiston.h>
#include <FDM/JSBSim/models/propulsion/FGTurbine.h>
cont = FGColumnVector3( contact[0], contact[1], contact[2] );
return agl;
}
+
+ virtual double GetTerrainGeoCentRadius(double t, const FGLocation& l) const {
+ double loc_cart[3] = { l(eX), l(eY), l(eZ) };
+ double contact[3], normal[3], vel[3], angularVel[3], agl = 0;
+ mInterface->get_agl_ft(t, loc_cart, SG_METER_TO_FEET*2, contact, normal,
+ vel, angularVel, &agl);
+ return sqrt(contact[0]*contact[0]+contact[1]*contact[1]+contact[2]*contact[2]);
+ }
+
+ virtual double GetSeaLevelRadius(const FGLocation& l) const {
+ double seaLevelRadius, latGeoc;
+
+ sgGeodToGeoc(l.GetGeodLatitudeRad(), l.GetGeodAltitude(),
+ &seaLevelRadius, &latGeoc);
+
+ return seaLevelRadius * SG_METER_TO_FEET;
+ }
+
+ virtual void SetTerrainGeoCentRadius(double radius) {}
+ virtual void SetSeaLevelRadius(double radius) {}
private:
FGJSBsim* mInterface;
};
+// FG uses a squared normalized magnitude for turbulence
+// this lookup table maps fg's severity levels
+// none(0), light(1/3), moderate(2/3) and severe(3/3)
+// to the POE table indexes 0, 3, 4 and 7
+class FGTurbulenceSeverityTable : public FGTable {
+public:
+ FGTurbulenceSeverityTable() : FGTable(4) {
+ *this << (0.0/9.0) << 0.0;
+ *this << (1.0/9.0) << 3.0;
+ *this << (4.0/9.0) << 4.0;
+ *this << (9.0/9.0) << 7.0;
+ }
+};
+
/******************************************************************************/
+std::map<std::string,int> FGJSBsim::TURBULENCE_TYPE_NAMES;
+
+static FGTurbulenceSeverityTable TurbulenceSeverityTable;
FGJSBsim::FGJSBsim( double dt )
: FGInterface(dt), got_wire(false)
{
bool result;
+ if( TURBULENCE_TYPE_NAMES.empty() ) {
+ TURBULENCE_TYPE_NAMES["ttNone"] = FGWinds::ttNone;
+ TURBULENCE_TYPE_NAMES["ttStandard"] = FGWinds::ttStandard;
+ TURBULENCE_TYPE_NAMES["ttCulp"] = FGWinds::ttCulp;
+ TURBULENCE_TYPE_NAMES["ttMilspec"] = FGWinds::ttMilspec;
+ TURBULENCE_TYPE_NAMES["ttTustin"] = FGWinds::ttTustin;
+ }
+
// Set up the debugging level
// FIXME: this will not respond to
// runtime changes
fdmex->SetGroundCallback( new FGFSGroundCallback(this) );
Atmosphere = fdmex->GetAtmosphere();
+ Winds = fdmex->GetWinds();
FCS = fdmex->GetFCS();
MassBalance = fdmex->GetMassBalance();
Propulsion = fdmex->GetPropulsion();
Aircraft = fdmex->GetAircraft();
- Propagate = fdmex->GetPropagate();
+ Propagate = fdmex->GetPropagate();
Auxiliary = fdmex->GetAuxiliary();
Inertial = fdmex->GetInertial();
Aerodynamics = fdmex->GetAerodynamics();
GroundReactions = fdmex->GetGroundReactions();
+ Accelerations = fdmex->GetAccelerations();
fgic=fdmex->GetIC();
needTrim=true;
// Set initial fuel levels if provided.
for (unsigned int i = 0; i < Propulsion->GetNumTanks(); i++) {
+ double d;
SGPropertyNode * node = fgGetNode("/consumables/fuel/tank", i, true);
- if (node->getChild("level-gal_us", 0, false) != 0) {
- Propulsion->GetTank(i)->SetContents(node->getDoubleValue("level-gal_us") * 6.6);
+ FGTank* tank = Propulsion->GetTank(i);
+
+ d = node->getNode( "density-ppg", true )->getDoubleValue();
+ if( d > 0.0 ) {
+ tank->SetDensity( d );
+ } else {
+ node->getNode( "density-ppg", true )->setDoubleValue( SG_MAX2<double>(tank->GetDensity(), 0.1) );
+ }
+
+ d = node->getNode( "level-lbs", true )->getDoubleValue();
+ if( d > 0.0 ) {
+ tank->SetContents( d );
} else {
- node->setDoubleValue("level-lbs", Propulsion->GetTank(i)->GetContents());
- node->setDoubleValue("level-gal_us", Propulsion->GetTank(i)->GetContents() / 6.6);
+ node->getNode( "level-lbs", true )->setDoubleValue( tank->GetContents() );
}
- node->setDoubleValue("capacity-gal_us",
- Propulsion->GetTank(i)->GetCapacity() / 6.6);
+ /* Capacity is read-only in FGTank and can't be overwritten from FlightGear */
+ node->getNode("capacity-gal_us", true )->setDoubleValue( tank->GetCapacityGallons() );
}
Propulsion->SetFuelFreeze((fgGetNode("/sim/freeze/fuel",true))->getBoolValue());
temperature = fgGetNode("/environment/temperature-degc",true);
pressure = fgGetNode("/environment/pressure-inhg",true);
- density = fgGetNode("/environment/density-slugft3",true);
+ pressureSL = fgGetNode("/environment/pressure-sea-level-inhg",true);
+ ground_wind = fgGetNode("/environment/config/boundary/entry[0]/wind-speed-kt",true);
turbulence_gain = fgGetNode("/environment/turbulence/magnitude-norm",true);
turbulence_rate = fgGetNode("/environment/turbulence/rate-hz",true);
+ turbulence_model = fgGetNode("/environment/params/jsbsim-turbulence-model",true);
wind_from_north= fgGetNode("/environment/wind-from-north-fps",true);
wind_from_east = fgGetNode("/environment/wind-from-east-fps" ,true);
fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-offset-x-in", 196),
fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-offset-y-in", 0),
fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-offset-z-in", -16));
+ last_hook_tip[0] = 0; last_hook_tip[1] = 0; last_hook_tip[2] = 0;
+ last_hook_root[0] = 0; last_hook_root[1] = 0; last_hook_root[2] = 0;
crashed = false;
}
FGJSBsim::~FGJSBsim(void)
{
delete fdmex;
-
- SGPropertyNode_ptr jsbsimRoot = fgGetNode("/fdm/jsbsim");
- if (jsbsimRoot) {
- SGPropertyNode* fdm = jsbsimRoot->getParent();
- fdm->removeChild("jsbsim", 0, false);
- }
- // properties are deleted when the sharedPtr above goes away
}
/******************************************************************************/
// init method first.
if (fgGetBool("/environment/params/control-fdm-atmosphere")) {
- Atmosphere->UseExternal();
- Atmosphere->SetExTemperature(
- 9.0/5.0*(temperature->getDoubleValue()+273.15) );
- Atmosphere->SetExPressure(pressure->getDoubleValue()*70.726566);
- Atmosphere->SetExDensity(density->getDoubleValue());
- Atmosphere->SetTurbType(FGAtmosphere::ttCulp);
- Atmosphere->SetTurbGain(turbulence_gain->getDoubleValue());
- Atmosphere->SetTurbRate(turbulence_rate->getDoubleValue());
-
- } else {
- Atmosphere->UseInternal();
+ Atmosphere->SetTemperature(temperature->getDoubleValue(), get_Altitude(), FGAtmosphere::eCelsius);
+ Atmosphere->SetPressureSL(pressureSL->getDoubleValue(), FGAtmosphere::eInchesHg);
+ // initialize to no turbulence, these values get set in the update loop
+ Winds->SetTurbType(FGWinds::ttNone);
+ Winds->SetTurbGain(0.0);
+ Winds->SetTurbRate(0.0);
+ Winds->SetWindspeed20ft(0.0);
+ Winds->SetProbabilityOfExceedence(0.0);
}
- fgic->SetVNorthFpsIC( -wind_from_north->getDoubleValue() );
- fgic->SetVEastFpsIC( -wind_from_east->getDoubleValue() );
- fgic->SetVDownFpsIC( -wind_from_down->getDoubleValue() );
-
- //Atmosphere->SetExTemperature(get_Static_temperature());
- //Atmosphere->SetExPressure(get_Static_pressure());
- //Atmosphere->SetExDensity(get_Density());
- SG_LOG(SG_FLIGHT,SG_INFO,"T,p,rho: " << fdmex->GetAtmosphere()->GetTemperature()
- << ", " << fdmex->GetAtmosphere()->GetPressure()
- << ", " << fdmex->GetAtmosphere()->GetDensity() );
-
-// deprecate egt_degf for egt-degf to have consistent naming
-// TODO: raise log-level to ALERT in summer 2010,
-// remove alias in fall 2010,
-// remove this code in winter 2010
- for (unsigned int i=0; i < Propulsion->GetNumEngines(); i++) {
- SGPropertyNode * node = fgGetNode("engines/engine", i, true);
- SGPropertyNode * egtn = node->getNode( "egt_degf" );
- if( egtn != NULL ) {
- SG_LOG(SG_FLIGHT,SG_WARN,
- "Aircraft uses deprecated node egt_degf. Please upgrade to egt-degf");
- node->getNode("egt-degf", true)->alias( egtn );
- }
- }
-// end of egt_degf deprecation patch
+ fgic->SetWindNEDFpsIC( -wind_from_north->getDoubleValue(),
+ -wind_from_east->getDoubleValue(),
+ -wind_from_down->getDoubleValue() );
- if (fgGetBool("/sim/presets/running")) {
- for (unsigned int i=0; i < Propulsion->GetNumEngines(); i++) {
- SGPropertyNode * node = fgGetNode("engines/engine", i, true);
- node->setBoolValue("running", true);
- Propulsion->GetEngine(i)->SetRunning(true);
- }
- }
+ SG_LOG(SG_FLIGHT,SG_INFO,"T,p,rho: " << Atmosphere->GetTemperature()
+ << ", " << Atmosphere->GetPressure()
+ << ", " << Atmosphere->GetDensity() );
FCS->SetDfPos( ofNorm, globals->get_controls()->get_flaps() );
+ needTrim = startup_trim->getBoolValue();
common_init();
copy_to_JSBsim();
fdmex->RunIC(); //loop JSBSim once w/o integrating
+ if (fgGetBool("/sim/presets/running")) {
+ Propulsion->InitRunning(-1);
+ for (unsigned int i = 0; i < Propulsion->GetNumEngines(); i++) {
+ FGPiston* eng = (FGPiston*)Propulsion->GetEngine(i);
+ globals->get_controls()->set_magnetos(i, eng->GetMagnetos());
+ globals->get_controls()->set_mixture(i, FCS->GetMixtureCmd(i));
+ }
+ }
+
+ if ( needTrim ) {
+ FGLocation cart(fgic->GetLongitudeRadIC(), fgic->GetLatitudeRadIC(),
+ get_Sea_level_radius() + fgic->GetAltitudeASLFtIC());
+ double cart_pos[3], contact[3], d[3], vel[3], agl;
+ update_ground_cache(cart, cart_pos, 0.01);
+
+ get_agl_ft(fdmex->GetSimTime(), cart_pos, SG_METER_TO_FEET*2, contact,
+ d, vel, d, &agl);
+ double terrain_alt = sqrt(contact[0]*contact[0] + contact[1]*contact[1]
+ + contact[2]*contact[2]) - get_Sea_level_radius();
+
+ SG_LOG(SG_FLIGHT, SG_INFO, "Ready to trim, terrain elevation is: "
+ << terrain_alt * SG_METER_TO_FEET );
+
+ if (fgGetBool("/sim/presets/onground")) {
+ FGColumnVector3 gndVelNED = cart.GetTec2l()
+ * FGColumnVector3(vel[0], vel[1], vel[2]);
+ fgic->SetVNorthFpsIC(gndVelNED(1));
+ fgic->SetVEastFpsIC(gndVelNED(2));
+ fgic->SetVDownFpsIC(gndVelNED(3));
+ }
+ fgic->SetTerrainElevationFtIC( terrain_alt );
+ do_trim();
+ needTrim = false;
+ }
+
copy_from_JSBsim(); //update the bus
SG_LOG( SG_FLIGHT, SG_INFO, " Initialized JSBSim with:" );
/******************************************************************************/
+void FGJSBsim::unbind()
+{
+ fdmex->Unbind();
+ FGInterface::unbind();
+}
+
+/******************************************************************************/
+
// Run an iteration of the EOM (equations of motion)
void FGJSBsim::update( double dt )
return;
int multiloop = _calc_multiloop(dt);
-
- int i;
-
- // Compute the radius of the aircraft. That is the radius of a ball
- // where all gear units are in. At the moment it is at least 10ft ...
- double acrad = 10.0;
- int n_gears = GroundReactions->GetNumGearUnits();
- for (i=0; i<n_gears; ++i) {
- FGColumnVector3 bl = GroundReactions->GetGearUnit(i)->GetBodyLocation();
- double r = bl.Magnitude();
- if (acrad < r)
- acrad = r;
- }
-
- // Compute the potential movement of this aircraft and query for the
- // ground in this area.
- double groundCacheRadius = acrad + 2*dt*Propagate->GetUVW().Magnitude();
- double alt, slr, lat, lon;
FGLocation cart = Auxiliary->GetLocationVRP();
- if ( needTrim && startup_trim->getBoolValue() ) {
- alt = fgic->GetAltitudeASLFtIC();
- slr = fgic->GetSeaLevelRadiusFtIC();
- lat = fgic->GetLatitudeDegIC() * SGD_DEGREES_TO_RADIANS;
- lon = fgic->GetLongitudeDegIC() * SGD_DEGREES_TO_RADIANS;
- cart = FGLocation(lon, lat, alt+slr);
- }
- double cart_pos[3] = { cart(1), cart(2), cart(3) };
- double t0 = fdmex->GetSimTime();
- bool cache_ok = prepare_ground_cache_ft( t0, t0 + dt, cart_pos,
- groundCacheRadius );
- if (!cache_ok) {
- SG_LOG(SG_FLIGHT, SG_WARN,
- "FGInterface is being called without scenery below the aircraft!");
-
- alt = fgic->GetAltitudeASLFtIC();
- SG_LOG(SG_FLIGHT, SG_WARN, "altitude = " << alt);
-
- slr = fgic->GetSeaLevelRadiusFtIC();
- SG_LOG(SG_FLIGHT, SG_WARN, "sea level radius = " << slr);
-
- lat = fgic->GetLatitudeDegIC() * SGD_DEGREES_TO_RADIANS;
- SG_LOG(SG_FLIGHT, SG_WARN, "latitude = " << lat);
-
- lon = fgic->GetLongitudeDegIC() * SGD_DEGREES_TO_RADIANS;
- SG_LOG(SG_FLIGHT, SG_WARN, "longitude = " << lon);
- //return;
- }
+ double cart_pos[3];
+
+ update_ground_cache(cart, cart_pos, dt);
copy_to_JSBsim();
trimmed->setBoolValue(false);
- if ( needTrim ) {
- if ( startup_trim->getBoolValue() ) {
- double contact[3], d[3], vel[3], agl;
- get_agl_ft(fdmex->GetSimTime(), cart_pos, SG_METER_TO_FEET*2, contact,
- d, vel, d, &agl);
- double terrain_alt = sqrt(contact[0]*contact[0] + contact[1]*contact[1]
- + contact[2]*contact[2]) - fgic->GetSeaLevelRadiusFtIC();
-
- SG_LOG(SG_FLIGHT, SG_INFO,
- "Ready to trim, terrain elevation is: "
- << terrain_alt * SG_METER_TO_FEET );
-
- if (fgGetBool("/sim/presets/onground")) {
- FGColumnVector3 gndVelNED = cart.GetTec2l()
- * FGColumnVector3(vel[0], vel[1], vel[2]);
- fgic->SetVNorthFpsIC(gndVelNED(1));
- fgic->SetVEastFpsIC(gndVelNED(2));
- fgic->SetVDownFpsIC(gndVelNED(3));
- }
- fgic->SetTerrainElevationFtIC( terrain_alt );
- do_trim();
- } else {
- fdmex->RunIC(); //apply any changes made through the set_ functions
- }
- needTrim = false;
- }
-
- for ( i=0; i < multiloop; i++ ) {
+ for ( int i=0; i < multiloop; i++ ) {
fdmex->Run();
- update_external_forces(fdmex->GetSimTime() + i * fdmex->GetDeltaT());
+ update_external_forces(fdmex->GetSimTime() + i * fdmex->GetDeltaT());
}
FGJSBBase::Message* msg;
- while (msg = fdmex->ProcessNextMessage()) {
+ while ((msg = fdmex->ProcessNextMessage()) != NULL) {
// msg = fdmex->ProcessNextMessage();
switch (msg->type) {
case FGJSBBase::Message::eText:
/******************************************************************************/
+void FGJSBsim::suspend()
+{
+ fdmex->Hold();
+ SGSubsystem::suspend();
+}
+
+/******************************************************************************/
+
+void FGJSBsim::resume()
+{
+ fdmex->Resume();
+ SGSubsystem::resume();
+}
+
+/******************************************************************************/
+
// Convert from the FGInterface struct to the JSBsim generic_ struct
bool FGJSBsim::copy_to_JSBsim()
{
- double tmp;
unsigned int i;
// copy control positions into the JSBsim structure
} // end FGTurbine code block
case FGEngine::etRocket:
{ // FGRocket code block
- FGRocket* eng = (FGRocket*)Propulsion->GetEngine(i);
+// FGRocket* eng = (FGRocket*)Propulsion->GetEngine(i);
break;
} // end FGRocket code block
case FGEngine::etTurboprop:
} // end FGEngine code block
}
+ Atmosphere->SetTemperature(temperature->getDoubleValue(), get_Altitude(), FGAtmosphere::eCelsius);
+ Atmosphere->SetPressureSL(pressureSL->getDoubleValue(), FGAtmosphere::eInchesHg);
- Propagate->SetSeaLevelRadius( get_Sea_level_radius() );
-
- Atmosphere->SetExTemperature(
- 9.0/5.0*(temperature->getDoubleValue()+273.15) );
- Atmosphere->SetExPressure(pressure->getDoubleValue()*70.726566);
- Atmosphere->SetExDensity(density->getDoubleValue());
-
- tmp = turbulence_gain->getDoubleValue();
- //Atmosphere->SetTurbGain(tmp * tmp * 100.0);
+ Winds->SetTurbType((FGWinds::tType)TURBULENCE_TYPE_NAMES[turbulence_model->getStringValue()]);
+ switch( Winds->GetTurbType() ) {
+ case FGWinds::ttStandard:
+ case FGWinds::ttCulp: {
+ double tmp = turbulence_gain->getDoubleValue();
+ Winds->SetTurbGain(tmp * tmp * 100.0);
+ Winds->SetTurbRate(turbulence_rate->getDoubleValue());
+ break;
+ }
+ case FGWinds::ttMilspec:
+ case FGWinds::ttTustin: {
+ // milspec turbulence: 3=light, 4=moderate, 6=severe turbulence
+ // turbulence_gain normalized: 0: none, 1/3: light, 2/3: moderate, 3/3: severe
+ double tmp = turbulence_gain->getDoubleValue();
+ Winds->SetProbabilityOfExceedence(
+ SGMiscd::roundToInt(TurbulenceSeverityTable.GetValue( tmp ) )
+ );
+ Winds->SetWindspeed20ft(ground_wind->getDoubleValue());
+ break;
+ }
- tmp = turbulence_rate->getDoubleValue();
- //Atmosphere->SetTurbRate(tmp);
+ default:
+ break;
+ }
- Atmosphere->SetWindNED( -wind_from_north->getDoubleValue(),
- -wind_from_east->getDoubleValue(),
- -wind_from_down->getDoubleValue() );
+ Winds->SetWindNED( -wind_from_north->getDoubleValue(),
+ -wind_from_east->getDoubleValue(),
+ -wind_from_down->getDoubleValue() );
// SG_LOG(SG_FLIGHT,SG_INFO, "Wind NED: "
// << get_V_north_airmass() << ", "
// << get_V_east_airmass() << ", "
for (i = 0; i < Propulsion->GetNumTanks(); i++) {
SGPropertyNode * node = fgGetNode("/consumables/fuel/tank", i, true);
FGTank * tank = Propulsion->GetTank(i);
- tank->SetContents(node->getDoubleValue("level-gal_us") * 6.6);
-// tank->SetContents(node->getDoubleValue("level-lbs"));
+ double fuelDensity = node->getDoubleValue("density-ppg");
+
+ if (fuelDensity < 0.1)
+ fuelDensity = 6.0; // Use average fuel value
+
+ tank->SetDensity(fuelDensity);
+ tank->SetContents(node->getDoubleValue("level-lbs"));
}
Propulsion->SetFuelFreeze((fgGetNode("/sim/freeze/fuel",true))->getBoolValue());
MassBalance->GetXYZcg(2),
MassBalance->GetXYZcg(3) );
- _set_Accels_Body( Aircraft->GetBodyAccel(1),
- Aircraft->GetBodyAccel(2),
- Aircraft->GetBodyAccel(3) );
+ _set_Accels_Body( Accelerations->GetBodyAccel(1),
+ Accelerations->GetBodyAccel(2),
+ Accelerations->GetBodyAccel(3) );
- _set_Accels_CG_Body_N ( Aircraft->GetNcg(1),
- Aircraft->GetNcg(2),
- Aircraft->GetNcg(3) );
+ _set_Accels_CG_Body_N ( Auxiliary->GetNcg(1),
+ Auxiliary->GetNcg(2),
+ Auxiliary->GetNcg(3) );
_set_Accels_Pilot_Body( Auxiliary->GetPilotAccel(1),
Auxiliary->GetPilotAccel(2),
Auxiliary->GetPilotAccel(3) );
- _set_Nlf( Aircraft->GetNlf() );
+ _set_Nlf( Auxiliary->GetNlf() );
// Velocities
// Positions of Visual Reference Point
FGLocation l = Auxiliary->GetLocationVRP();
- _updateGeocentricPosition( l.GetLatitude(), l.GetLongitude(),
- l.GetRadius() - get_Sea_level_radius() );
+ _updatePosition(SGGeoc::fromRadFt( l.GetLongitude(), l.GetLatitude(),
+ l.GetRadius() ));
_set_Altitude_AGL( Propagate->GetDistanceAGL() );
{
_set_Gamma_vert_rad( Auxiliary->GetGamma() );
- _set_Earth_position_angle( Inertial->GetEarthPositionAngle() );
+ _set_Earth_position_angle( Propagate->GetEarthPositionAngle() );
_set_Climb_Rate( Propagate->Gethdot() );
break;
case FGEngine::etRocket:
{ // FGRocket code block
- FGRocket* eng = (FGRocket*)Propulsion->GetEngine(i);
+// FGRocket* eng = (FGRocket*)Propulsion->GetEngine(i);
} // end FGRocket code block
break;
case FGEngine::etTurbine:
node->setDoubleValue("egt-degf", 32 + eng->GetEGT()*9/5);
node->setBoolValue("augmentation", eng->GetAugmentation());
node->setBoolValue("water-injection", eng->GetInjection());
- node->setBoolValue("ignition", eng->GetIgnition());
+ node->setBoolValue("ignition", eng->GetIgnition() != 0);
node->setDoubleValue("nozzle-pos-norm", eng->GetNozzle());
node->setDoubleValue("inlet-pos-norm", eng->GetInlet());
node->setDoubleValue("oil-pressure-psi", eng->getOilPressure_psi());
node->setDoubleValue("n1", eng->GetN1());
//node->setDoubleValue("n2", eng->GetN2());
node->setDoubleValue("itt_degf", 32 + eng->GetITT()*9/5);
- node->setBoolValue("ignition", eng->GetIgnition());
+ node->setBoolValue("ignition", eng->GetIgnition() != 0);
node->setDoubleValue("nozzle-pos-norm", eng->GetNozzle());
node->setDoubleValue("inlet-pos-norm", eng->GetInlet());
node->setDoubleValue("oil-pressure-psi", eng->getOilPressure_psi());
node->setBoolValue("cutoff", eng->GetCutoff());
node->setBoolValue("starting", eng->GetEngStarting());
node->setBoolValue("generator-power", eng->GetGeneratorPower());
- node->setBoolValue("damaged", eng->GetCondition());
+ node->setBoolValue("damaged", eng->GetCondition() != 0);
node->setBoolValue("ielu-intervent", eng->GetIeluIntervent());
node->setDoubleValue("oil-temperature-degf", eng->getOilTemp_degF());
// node->setBoolValue("onfire", eng->GetFire());
switch (thruster->GetType()) {
case FGThruster::ttNozzle:
{ // FGNozzle code block
- FGNozzle* noz = (FGNozzle*)thruster;
+// FGNozzle* noz = (FGNozzle*)thruster;
} // end FGNozzle code block
break;
case FGThruster::ttPropeller:
break;
case FGThruster::ttRotor:
{ // FGRotor code block
- FGRotor* rotor = (FGRotor*)thruster;
+// FGRotor* rotor = (FGRotor*)thruster;
} // end FGRotor code block
break;
case FGThruster::ttDirect:
FGTank* tank = Propulsion->GetTank(i);
double contents = tank->GetContents();
double temp = tank->GetTemperature_degC();
- node->setDoubleValue("level-gal_us", contents/6.6);
+ double fuelDensity = tank->GetDensity();
+
+ if (fuelDensity < 0.1)
+ fuelDensity = 6.0; // Use average fuel value
+
+ node->setDoubleValue("density-ppg" , fuelDensity);
node->setDoubleValue("level-lbs", contents);
if (temp != -9999.0) node->setDoubleValue("temperature_degC", temp);
}
//Positions
void FGJSBsim::set_Latitude(double lat)
{
- static SGConstPropertyNode_ptr altitude = fgGetNode("/position/altitude-ft");
- double alt;
- double sea_level_radius_meters, lat_geoc;
+ static SGConstPropertyNode_ptr altitude = fgGetNode("/position/altitude-ft");
+ double alt = altitude->getDoubleValue();
+ double sea_level_radius_meters, lat_geoc;
- // In case we're not trimming
- FGInterface::set_Latitude(lat);
+ if ( alt < -9990 ) alt = 0.0;
- if ( altitude->getDoubleValue() > -9990 ) {
- alt = altitude->getDoubleValue();
- } else {
- alt = 0.0;
- }
+ SG_LOG(SG_FLIGHT,SG_INFO,"FGJSBsim::set_Latitude: " << lat );
+ SG_LOG(SG_FLIGHT,SG_INFO," cur alt (ft) = " << alt );
+
+ sgGeodToGeoc( lat, alt * SG_FEET_TO_METER,
+ &sea_level_radius_meters, &lat_geoc );
- update_ic();
- SG_LOG(SG_FLIGHT,SG_INFO,"FGJSBsim::set_Latitude: " << lat );
- SG_LOG(SG_FLIGHT,SG_INFO," cur alt (ft) = " << alt );
+ double sea_level_radius_ft = sea_level_radius_meters * SG_METER_TO_FEET;
+ _set_Sea_level_radius( sea_level_radius_ft );
- sgGeodToGeoc( lat, alt * SG_FEET_TO_METER,
- &sea_level_radius_meters, &lat_geoc );
- _set_Sea_level_radius( sea_level_radius_meters * SG_METER_TO_FEET );
- fgic->SetSeaLevelRadiusFtIC( sea_level_radius_meters * SG_METER_TO_FEET );
+ if (needTrim) {
+ fgic->SetSeaLevelRadiusFtIC( sea_level_radius_ft );
fgic->SetLatitudeRadIC( lat_geoc );
- needTrim=true;
+ }
+ else
+ Propagate->SetLatitude(lat_geoc);
+
+ FGInterface::set_Latitude(lat);
}
void FGJSBsim::set_Longitude(double lon)
{
- SG_LOG(SG_FLIGHT,SG_INFO,"FGJSBsim::set_Longitude: " << lon );
+ SG_LOG(SG_FLIGHT,SG_INFO,"FGJSBsim::set_Longitude: " << lon );
- // In case we're not trimming
- FGInterface::set_Longitude(lon);
+ if (needTrim)
+ fgic->SetLongitudeRadIC(lon);
+ else
+ Propagate->SetLongitude(lon);
- update_ic();
- fgic->SetLongitudeRadIC( lon );
- needTrim=true;
+ FGInterface::set_Longitude(lon);
}
// Sets the altitude above sea level.
void FGJSBsim::set_Altitude(double alt)
{
- static SGConstPropertyNode_ptr latitude = fgGetNode("/position/latitude-deg");
+ SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Altitude: " << alt );
- double sea_level_radius_meters,lat_geoc;
-
- SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Altitude: " << alt );
- SG_LOG(SG_FLIGHT,SG_INFO, " lat (deg) = " << latitude->getDoubleValue() );
-
- // In case we're not trimming
- FGInterface::set_Altitude(alt);
-
- update_ic();
- sgGeodToGeoc( latitude->getDoubleValue() * SGD_DEGREES_TO_RADIANS, alt,
- &sea_level_radius_meters, &lat_geoc);
- _set_Sea_level_radius( sea_level_radius_meters * SG_METER_TO_FEET );
- fgic->SetSeaLevelRadiusFtIC( sea_level_radius_meters * SG_METER_TO_FEET );
- SG_LOG(SG_FLIGHT, SG_INFO,
- "Terrain elevation: " << FGInterface::get_Runway_altitude() * SG_METER_TO_FEET );
- fgic->SetLatitudeRadIC( lat_geoc );
+ if (needTrim)
fgic->SetAltitudeASLFtIC(alt);
- needTrim=true;
+ else
+ Propagate->SetAltitudeASL(alt);
+
+ FGInterface::set_Altitude(alt);
}
void FGJSBsim::set_V_calibrated_kts(double vc)
{
SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_V_calibrated_kts: " << vc );
- // In case we're not trimming
- FGInterface::set_V_calibrated_kts(vc);
-
- update_ic();
+ if (needTrim)
fgic->SetVcalibratedKtsIC(vc);
- needTrim=true;
+ else {
+ double p=pressure->getDoubleValue();
+ double psl=fdmex->GetAtmosphere()->GetPressureSL();
+ double rhosl=fdmex->GetAtmosphere()->GetDensitySL();
+ double mach = FGJSBBase::MachFromVcalibrated(vc, p, psl, rhosl);
+ double temp = 1.8*(temperature->getDoubleValue()+273.15);
+ double soundSpeed = sqrt(1.4*1716.0*temp);
+ FGColumnVector3 vUVW = Propagate->GetUVW();
+ vUVW.Normalize();
+ vUVW *= mach * soundSpeed;
+ Propagate->SetUVW(1, vUVW(1));
+ Propagate->SetUVW(2, vUVW(2));
+ Propagate->SetUVW(3, vUVW(3));
+ }
+
+ FGInterface::set_V_calibrated_kts(vc);
}
void FGJSBsim::set_Mach_number(double mach)
{
- SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Mach_number: " << mach );
+ SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Mach_number: " << mach );
- // In case we're not trimming
- FGInterface::set_Mach_number(mach);
-
- update_ic();
+ if (needTrim)
fgic->SetMachIC(mach);
- needTrim=true;
+ else {
+ double temp = 1.8*(temperature->getDoubleValue()+273.15);
+ double soundSpeed = sqrt(1.4*1716.0*temp);
+ FGColumnVector3 vUVW = Propagate->GetUVW();
+ vUVW.Normalize();
+ vUVW *= mach * soundSpeed;
+ Propagate->SetUVW(1, vUVW(1));
+ Propagate->SetUVW(2, vUVW(2));
+ Propagate->SetUVW(3, vUVW(3));
+ }
+
+ FGInterface::set_Mach_number(mach);
}
void FGJSBsim::set_Velocities_Local( double north, double east, double down )
{
- SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Velocities_Local: "
- << north << ", " << east << ", " << down );
-
- // In case we're not trimming
- FGInterface::set_Velocities_Local(north, east, down);
+ SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Velocities_Local: "
+ << north << ", " << east << ", " << down );
- update_ic();
+ if (needTrim) {
fgic->SetVNorthFpsIC(north);
fgic->SetVEastFpsIC(east);
fgic->SetVDownFpsIC(down);
- needTrim=true;
+ }
+ else {
+ FGColumnVector3 vNED(north, east, down);
+ FGColumnVector3 vUVW = Propagate->GetTl2b() * vNED;
+ Propagate->SetUVW(1, vUVW(1));
+ Propagate->SetUVW(2, vUVW(2));
+ Propagate->SetUVW(3, vUVW(3));
+ }
+
+ FGInterface::set_Velocities_Local(north, east, down);
}
void FGJSBsim::set_Velocities_Wind_Body( double u, double v, double w)
{
- SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Velocities_Wind_Body: "
- << u << ", " << v << ", " << w );
+ SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Velocities_Wind_Body: "
+ << u << ", " << v << ", " << w );
- // In case we're not trimming
- FGInterface::set_Velocities_Wind_Body(u, v, w);
-
- update_ic();
+ if (needTrim) {
fgic->SetUBodyFpsIC(u);
fgic->SetVBodyFpsIC(v);
fgic->SetWBodyFpsIC(w);
- needTrim=true;
+ }
+ else {
+ Propagate->SetUVW(1, u);
+ Propagate->SetUVW(2, v);
+ Propagate->SetUVW(3, w);
+ }
+
+ FGInterface::set_Velocities_Wind_Body(u, v, w);
}
//Euler angles
void FGJSBsim::set_Euler_Angles( double phi, double theta, double psi )
{
- SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Euler_Angles: "
- << phi << ", " << theta << ", " << psi );
-
- // In case we're not trimming
- FGInterface::set_Euler_Angles(phi, theta, psi);
+ SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Euler_Angles: "
+ << phi << ", " << theta << ", " << psi );
- update_ic();
+ if (needTrim) {
fgic->SetThetaRadIC(theta);
fgic->SetPhiRadIC(phi);
fgic->SetPsiRadIC(psi);
- needTrim=true;
+ }
+ else {
+ FGQuaternion quat(phi, theta, psi);
+ FGMatrix33 Tl2b = quat.GetT();
+ FGMatrix33 Ti2b = Tl2b*Propagate->GetTi2l();
+ FGQuaternion Qi = Ti2b.GetQuaternion();
+ Propagate->SetInertialOrientation(Qi);
+ }
+
+ FGInterface::set_Euler_Angles(phi, theta, psi);
}
//Flight Path
void FGJSBsim::set_Climb_Rate( double roc)
{
- SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Climb_Rate: " << roc );
+ SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Climb_Rate: " << roc );
- // In case we're not trimming
- FGInterface::set_Climb_Rate(roc);
-
- update_ic();
- //since both climb rate and flight path angle are set in the FG
- //startup sequence, something is needed to keep one from cancelling
- //out the other.
- if( !(fabs(roc) > 1 && fabs(fgic->GetFlightPathAngleRadIC()) < 0.01) ) {
+ //since both climb rate and flight path angle are set in the FG
+ //startup sequence, something is needed to keep one from cancelling
+ //out the other.
+ if( !(fabs(roc) > 1 && fabs(fgic->GetFlightPathAngleRadIC()) < 0.01) ) {
+ if (needTrim)
fgic->SetClimbRateFpsIC(roc);
+ else {
+ FGColumnVector3 vNED = Propagate->GetVel();
+ vNED(FGJSBBase::eDown) = -roc;
+ FGColumnVector3 vUVW = Propagate->GetTl2b() * vNED;
+ Propagate->SetUVW(1, vUVW(1));
+ Propagate->SetUVW(2, vUVW(2));
+ Propagate->SetUVW(3, vUVW(3));
}
- needTrim=true;
+
+ FGInterface::set_Climb_Rate(roc);
+ }
}
void FGJSBsim::set_Gamma_vert_rad( double gamma)
{
- SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Gamma_vert_rad: " << gamma );
+ SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Gamma_vert_rad: " << gamma );
- update_ic();
- if( !(fabs(gamma) < 0.01 && fabs(fgic->GetClimbRateFpsIC()) > 1) ) {
+ if( !(fabs(gamma) < 0.01 && fabs(fgic->GetClimbRateFpsIC()) > 1) ) {
+ if (needTrim)
fgic->SetFlightPathAngleRadIC(gamma);
+ else {
+ FGColumnVector3 vNED = Propagate->GetVel();
+ double vt = vNED.Magnitude();
+ vNED(FGJSBBase::eDown) = -vt * sin(gamma);
+ FGColumnVector3 vUVW = Propagate->GetTl2b() * vNED;
+ Propagate->SetUVW(1, vUVW(1));
+ Propagate->SetUVW(2, vUVW(2));
+ Propagate->SetUVW(3, vUVW(3));
}
- needTrim=true;
+
+ FGInterface::set_Gamma_vert_rad(gamma);
+ }
}
void FGJSBsim::init_gear(void )
{
fgtrim = new FGTrim(fdmex,tGround);
} else {
- fgtrim = new FGTrim(fdmex,tLongitudinal);
+ fgtrim = new FGTrim(fdmex,tFull);
}
if ( !fgtrim->DoTrim() ) {
pitch_trim->setDoubleValue( FCS->GetPitchTrimCmd() );
throttle_trim->setDoubleValue( FCS->GetThrottleCmd(0) );
aileron_trim->setDoubleValue( FCS->GetDaCmd() );
- rudder_trim->setDoubleValue( FCS->GetDrCmd() );
+ rudder_trim->setDoubleValue( -FCS->GetDrCmd() );
globals->get_controls()->set_elevator_trim(FCS->GetPitchTrimCmd());
globals->get_controls()->set_elevator(FCS->GetDeCmd());
- globals->get_controls()->set_throttle(FGControls::ALL_ENGINES,
- FCS->GetThrottleCmd(0));
+ for( unsigned i = 0; i < Propulsion->GetNumEngines(); i++ )
+ globals->get_controls()->set_throttle(i, FCS->GetThrottleCmd(i));
globals->get_controls()->set_aileron(FCS->GetDaCmd());
- globals->get_controls()->set_rudder( FCS->GetDrCmd());
+ globals->get_controls()->set_rudder( -FCS->GetDrCmd());
SG_LOG( SG_FLIGHT, SG_INFO, " Trim complete" );
}
-void FGJSBsim::update_ic(void)
+bool FGJSBsim::update_ground_cache(FGLocation cart, double* cart_pos, double dt)
{
- if ( !needTrim ) {
- fgic->SetLatitudeRadIC(get_Lat_geocentric() );
- fgic->SetLongitudeRadIC( get_Longitude() );
- fgic->SetAltitudeASLFtIC( get_Altitude() );
- fgic->SetVcalibratedKtsIC( get_V_calibrated_kts() );
- fgic->SetThetaRadIC( get_Theta() );
- fgic->SetPhiRadIC( get_Phi() );
- fgic->SetPsiRadIC( get_Psi() );
- fgic->SetClimbRateFpsIC( get_Climb_Rate() );
- }
+ // Compute the radius of the aircraft. That is the radius of a ball
+ // where all gear units are in. At the moment it is at least 10ft ...
+ double acrad = 10.0;
+ int n_gears = GroundReactions->GetNumGearUnits();
+ for (int i=0; i<n_gears; ++i) {
+ FGColumnVector3 bl = GroundReactions->GetGearUnit(i)->GetBodyLocation();
+ double r = bl.Magnitude();
+ if (acrad < r)
+ acrad = r;
+ }
+
+ // Compute the potential movement of this aircraft and query for the
+ // ground in this area.
+ double groundCacheRadius = acrad + 2*dt*Propagate->GetUVW().Magnitude();
+ cart_pos[0] = cart(1);
+ cart_pos[1] = cart(2);
+ cart_pos[2] = cart(3);
+ double t0 = fdmex->GetSimTime();
+ bool cache_ok = prepare_ground_cache_ft( t0, t0 + dt, cart_pos,
+ groundCacheRadius );
+ if (!cache_ok) {
+ SG_LOG(SG_FLIGHT, SG_WARN,
+ "FGInterface is being called without scenery below the aircraft!");
+
+ SG_LOG(SG_FLIGHT, SG_WARN, "altitude = "
+ << fgic->GetAltitudeASLFtIC());
+
+ SG_LOG(SG_FLIGHT, SG_WARN, "sea level radius = "
+ << get_Sea_level_radius());
+
+ SG_LOG(SG_FLIGHT, SG_WARN, "latitude = "
+ << fgic->GetLatitudeRadIC());
+
+ SG_LOG(SG_FLIGHT, SG_WARN, "longitude = "
+ << fgic->GetLongitudeRadIC());
+ }
+
+ return cache_ok;
}
bool
return true;
}
-inline static double dot3(const FGColumnVector3& a, const FGColumnVector3& b)
-{
- return a(1) * b(1) + a(2) * b(2) + a(3) * b(3);
-}
-
inline static double sqr(double x)
{
return x * x;
static void check_hook_solution(const FGColumnVector3& ground_normal_body, double E, double hook_length, double sin_fi_guess, double cos_fi_guess, double* sin_fis, double* cos_fis, double* fis, int* points)
{
FGColumnVector3 tip(-hook_length * cos_fi_guess, 0, hook_length * sin_fi_guess);
- double dist = dot3(tip, ground_normal_body);
+ double dist = DotProduct(tip, ground_normal_body);
if (fabs(dist + E) < 0.0001) {
sin_fis[*points] = sin_fi_guess;
cos_fis[*points] = cos_fi_guess;
if (got && root_agl_ft > 0 && root_agl_ft < hook_length) {
FGColumnVector3 ground_normal_body = Tl2b * (Tec2l * FGColumnVector3(ground_normal[0], ground_normal[1], ground_normal[2]));
FGColumnVector3 contact_body = Tl2b * Location.LocationToLocal(FGColumnVector3(contact[0], contact[1], contact[2]));
- double D = -dot3(contact_body, ground_normal_body);
+ double D = -DotProduct(contact_body, ground_normal_body);
// check hook tip agl against same ground plane
- double hook_tip_agl_ft = dot3(hook_tip_body, ground_normal_body) + D;
+ double hook_tip_agl_ft = DotProduct(hook_tip_body, ground_normal_body) + D;
if (hook_tip_agl_ft < 0) {
// hook tip: hx - l cos, hy, hz + l sin
// on ground: - n0 l cos + n2 l sin + E = 0
- double E = D + dot3(hook_root_body, ground_normal_body);
+ double E = D + DotProduct(hook_root_body, ground_normal_body);
// substitue x = sin fi, cos fi = sqrt(1 - x * x)
// and rearrange to get a quadratic with coeffs:
FGColumnVector3 wire_end2_body = Tl2b * Location.LocationToLocal(FGColumnVector3(wire_ends_ec[1][0], wire_ends_ec[1][1], wire_ends_ec[1][2])) - hook_root_body;
FGColumnVector3 force_plane_normal = wire_end1_body * wire_end2_body;
force_plane_normal.Normalize();
- cos_fi = dot3(force_plane_normal, FGColumnVector3(0, 0, 1));
+ cos_fi = DotProduct(force_plane_normal, FGColumnVector3(0, 0, 1));
if (cos_fi < 0) cos_fi = -cos_fi;
sin_fi = sqrt(1 - sqr(cos_fi));
fi = atan2(sin_fi, cos_fi) * SG_RADIANS_TO_DEGREES;
projects / flightgear.git / blobdiff