src/FDM/JSBSim/JSBSim.cxx

   1 // JSBsim.cxx -- interface to the JSBsim flight model
   2 //
   3 // Written by Curtis Olson, started February 1999.
   4 //
   5 // Copyright (C) 1999  Curtis L. Olson  - curt@flightgear.org
   6 //
   7 // This program is free software; you can redistribute it and/or
   8 // modify it under the terms of the GNU Lesser General Public License as
   9 // published by the Free Software Foundation; either version 2 of the
  10 // License, or (at your option) any later version.
  11 //
  12 // This program is distributed in the hope that it will be useful, but
  13 // WITHOUT ANY WARRANTY; without even the implied warranty of
  14 // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
  15 // Lesser General Public License for more details.
  16 //
  17 // You should have received a copy of the GNU Lesser General Public License
  18 // along with this program; if not, write to the Free Software
  19 // Foundation, Inc., 51 Franklin St, Fifth Floor, Boston, MA  02110-1301, USA.
  20 //
  21 // $Id: FlightGear.cxx,v 1.15 2014/01/28 09:42:20 ehofman Exp $
  22
  23
  24 #ifdef HAVE_CONFIG_H
  25 #  include <config.h>
  26 #endif
  27
  28 #include <simgear/compiler.h>
  29 #include <simgear/sg_inlines.h>
  30
  31 #include <cstdlib>    //    size_t
  32 #include <string>
  33
  34 #include <simgear/constants.h>
  35 #include <simgear/debug/logstream.hxx>
  36 #include <simgear/math/sg_geodesy.hxx>
  37 #include <simgear/misc/sg_path.hxx>
  38 #include <simgear/structure/commands.hxx>
  39 #include <simgear/bvh/BVHMaterial.hxx>
  40
  41 #include <FDM/flight.hxx>
  42
  43 #include <Aircraft/controls.hxx>
  44 #include <Main/globals.hxx>
  45 #include <Main/fg_props.hxx>
  46
  47 #include "JSBSim.hxx"
  48 #include <FDM/JSBSim/FGFDMExec.h>
  49 #include <FDM/JSBSim/FGJSBBase.h>
  50 #include <FDM/JSBSim/initialization/FGInitialCondition.h>
  51 #include <FDM/JSBSim/initialization/FGTrim.h>
  52 #include <FDM/JSBSim/models/FGModel.h>
  53 #include <FDM/JSBSim/models/FGAircraft.h>
  54 #include <FDM/JSBSim/models/FGFCS.h>
  55 #include <FDM/JSBSim/models/FGPropagate.h>
  56 #include <FDM/JSBSim/models/FGAuxiliary.h>
  57 #include <FDM/JSBSim/models/FGInertial.h>
  58 #include <FDM/JSBSim/models/FGAtmosphere.h>
  59 #include <FDM/JSBSim/models/FGMassBalance.h>
  60 #include <FDM/JSBSim/models/FGAerodynamics.h>
  61 #include <FDM/JSBSim/models/FGLGear.h>
  62 #include <FDM/JSBSim/models/FGGroundReactions.h>
  63 #include <FDM/JSBSim/models/FGPropulsion.h>
  64 #include <FDM/JSBSim/models/FGAccelerations.h>
  65 #include <FDM/JSBSim/models/atmosphere/FGWinds.h>
  66 #include <FDM/JSBSim/models/propulsion/FGEngine.h>
  67 #include <FDM/JSBSim/models/propulsion/FGPiston.h>
  68 #include <FDM/JSBSim/models/propulsion/FGTurbine.h>
  69 #include <FDM/JSBSim/models/propulsion/FGTurboProp.h>
  70 #include <FDM/JSBSim/models/propulsion/FGRocket.h>
  71 #include <FDM/JSBSim/models/propulsion/FGElectric.h>
  72 #include <FDM/JSBSim/models/propulsion/FGNozzle.h>
  73 #include <FDM/JSBSim/models/propulsion/FGPropeller.h>
  74 #include <FDM/JSBSim/models/propulsion/FGRotor.h>
  75 #include <FDM/JSBSim/models/propulsion/FGTank.h>
  76 #include <FDM/JSBSim/input_output/FGPropertyManager.h>
  77 #include <FDM/JSBSim/input_output/FGGroundCallback.h>
  78
  79 using namespace JSBSim;
  80
  81 static inline double
  82 FMAX (double a, double b)
  83 {
  84   return a > b ? a : b;
  85 }
  86
  87 class FGFSGroundCallback : public FGGroundCallback {
  88 public:
  89   FGFSGroundCallback(FGJSBsim* ifc) : mInterface(ifc) {}
  90   virtual ~FGFSGroundCallback() {}
  91
  92   /** Get the altitude above sea level dependent on the location. */
  93   virtual double GetAltitude(const FGLocation& l) const {
  94     double pt[3] = { SG_FEET_TO_METER*l(FGJSBBase::eX),
  95                      SG_FEET_TO_METER*l(FGJSBBase::eY),
  96                      SG_FEET_TO_METER*l(FGJSBBase::eZ) };
  97     double lat, lon, alt;
  98     sgCartToGeod( pt, &lat, &lon, &alt);
  99     return alt * SG_METER_TO_FEET;
 100   }
 101
 102   /** Compute the altitude above ground. */
 103   virtual double GetAGLevel(double t, const FGLocation& l,
 104                             FGLocation& cont, FGColumnVector3& n,
 105                             FGColumnVector3& v, FGColumnVector3& w) const {
 106     double loc_cart[3] = { l(FGJSBBase::eX), l(FGJSBBase::eY), l(FGJSBBase::eZ) };
 107     double contact[3], normal[3], vel[3], angularVel[3], agl = 0;
 108     mInterface->get_agl_ft(t, loc_cart, SG_METER_TO_FEET*2, contact, normal,
 109                            vel, angularVel, &agl);
 110     n = FGColumnVector3( normal[0], normal[1], normal[2] );
 111     v = FGColumnVector3( vel[0], vel[1], vel[2] );
 112     w = FGColumnVector3( angularVel[0], angularVel[1], angularVel[2] );
 113     cont = FGColumnVector3( contact[0], contact[1], contact[2] );
 114     return agl;
 115   }
 116
 117   virtual double GetTerrainGeoCentRadius(double t, const FGLocation& l) const {
 118     double loc_cart[3] = { l(FGJSBBase::eX), l(FGJSBBase::eY), l(FGJSBBase::eZ) };
 119     double contact[3], normal[3], vel[3], angularVel[3], agl = 0;
 120     mInterface->get_agl_ft(t, loc_cart, SG_METER_TO_FEET*2, contact, normal,
 121                            vel, angularVel, &agl);
 122     return sqrt(contact[0]*contact[0]+contact[1]*contact[1]+contact[2]*contact[2]);
 123   }
 124
 125   virtual double GetSeaLevelRadius(const FGLocation& l) const {
 126     double seaLevelRadius, latGeoc;
 127
 128     sgGeodToGeoc(l.GetGeodLatitudeRad(), l.GetGeodAltitude(),
 129                  &seaLevelRadius, &latGeoc);
 130
 131     return seaLevelRadius * SG_METER_TO_FEET;
 132   }
 133
 134   virtual void SetTerrainGeoCentRadius(double radius) {}
 135   virtual void SetSeaLevelRadius(double radius) {}
 136 private:
 137   FGJSBsim* mInterface;
 138 };
 139
 140 // FG uses a squared normalized magnitude for turbulence
 141 // this lookup table maps fg's severity levels
 142 // none(0), light(1/3), moderate(2/3) and severe(3/3)
 143 // to the POE table indexes 0, 3, 4 and 7
 144 class FGTurbulenceSeverityTable : public FGTable {
 145 public:
 146   FGTurbulenceSeverityTable() : FGTable(4) {
 147     *this << (0.0/9.0) << 0.0;
 148     *this << (1.0/9.0) << 3.0;
 149     *this << (4.0/9.0) << 4.0;
 150     *this << (9.0/9.0) << 7.0;
 151   }
 152 };
 153
 154 /******************************************************************************/
 155 std::map<std::string,int> FGJSBsim::TURBULENCE_TYPE_NAMES;
 156
 157 static FGTurbulenceSeverityTable TurbulenceSeverityTable;
 158
 159 FGJSBsim::FGJSBsim( double dt )
 160   : FGInterface(dt), got_wire(false)
 161 {
 162     bool result;
 163     if( TURBULENCE_TYPE_NAMES.empty() ) {
 164         TURBULENCE_TYPE_NAMES["ttNone"]     = FGWinds::ttNone;
 165         TURBULENCE_TYPE_NAMES["ttStandard"] = FGWinds::ttStandard;
 166         TURBULENCE_TYPE_NAMES["ttCulp"]     = FGWinds::ttCulp;
 167         TURBULENCE_TYPE_NAMES["ttMilspec"]  = FGWinds::ttMilspec;
 168         TURBULENCE_TYPE_NAMES["ttTustin"]   = FGWinds::ttTustin;
 169     }
 170
 171     // Set up the debugging level
 172     // FIXME: this will not respond to
 173     // runtime changes
 174
 175     if ((sglog().get_log_classes() & SG_FLIGHT) != 0) {
 176
 177                                 // do a rough-and-ready mapping to
 178                                 // the levels documented in FGFDMExec.h
 179         switch (sglog().get_log_priority()) {
 180         case SG_BULK:
 181             FGJSBBase::debug_lvl = 0x1f;
 182             break;
 183         case SG_DEBUG:
 184             FGJSBBase::debug_lvl = 0x1f;
 185         case SG_INFO:
 186         case SG_WARN:
 187         case SG_ALERT:
 188             FGJSBBase::debug_lvl = 0x00;
 189             break;
 190         }
 191     } else {
 192                                 // if flight is excluded, don't bother
 193             FGJSBBase::debug_lvl = 0x00;
 194     }
 195
 196     PropertyManager = new FGPropertyManager( (FGPropertyNode*)globals->get_props() );
 197     fdmex = new FGFDMExec( PropertyManager );
 198
 199     // Register ground callback.
 200     fdmex->SetGroundCallback( new FGFSGroundCallback(this) );
 201
 202     Atmosphere      = fdmex->GetAtmosphere();
 203     Winds           = fdmex->GetWinds();
 204     FCS             = fdmex->GetFCS();
 205     MassBalance     = fdmex->GetMassBalance();
 206     Propulsion      = fdmex->GetPropulsion();
 207     Aircraft        = fdmex->GetAircraft();
 208     Propagate       = fdmex->GetPropagate();
 209     Auxiliary       = fdmex->GetAuxiliary();
 210     Inertial        = fdmex->GetInertial();
 211     Aerodynamics    = fdmex->GetAerodynamics();
 212     GroundReactions = fdmex->GetGroundReactions();
 213     Accelerations   = fdmex->GetAccelerations();
 214
 215     fgic=fdmex->GetIC();
 216     needTrim=true;
 217
 218     SGPath aircraft_path( fgGetString("/sim/aircraft-dir") );
 219
 220     SGPath engine_path( fgGetString("/sim/fg-root") );
 221     engine_path.append( "Aircraft/Generic/JSBSim/Engines" );
 222
 223     SGPath systems_path( fgGetString("/sim/fg-root") );
 224     systems_path.append( "Aircraft/Generic/JSBSim/Systems" );
 225
 226 // deprecate sim-time-sec for simulation/sim-time-sec
 227 // remove alias with increased configuration file version number (2.1 or later)
 228     SGPropertyNode * node = fgGetNode("/fdm/jsbsim/simulation/sim-time-sec");
 229     fgGetNode("/fdm/jsbsim/sim-time-sec", true)->alias( node );
 230 // end of sim-time-sec deprecation patch
 231
 232     fdmex->Setdt( dt );
 233
 234     result = fdmex->LoadModel( aircraft_path.str(),
 235                                engine_path.str(),
 236                                systems_path.str(),
 237                                fgGetString("/sim/aero"), false );
 238
 239     if (result) {
 240       SG_LOG( SG_FLIGHT, SG_INFO, "  loaded aero.");
 241     } else {
 242       SG_LOG( SG_FLIGHT, SG_INFO,
 243               "  aero does not exist (you may have mis-typed the name).");
 244       throw(-1);
 245     }
 246
 247     SG_LOG( SG_FLIGHT, SG_INFO, "" );
 248     SG_LOG( SG_FLIGHT, SG_INFO, "" );
 249     SG_LOG( SG_FLIGHT, SG_INFO, "After loading aero definition file ..." );
 250
 251     int Neng = Propulsion->GetNumEngines();
 252     SG_LOG( SG_FLIGHT, SG_INFO, "num engines = " << Neng );
 253
 254     if ( GroundReactions->GetNumGearUnits() <= 0 ) {
 255         SG_LOG( SG_FLIGHT, SG_ALERT, "num gear units = "
 256                 << GroundReactions->GetNumGearUnits() );
 257         SG_LOG( SG_FLIGHT, SG_ALERT, "This is a very bad thing because with 0 gear units, the ground trimming");
 258         SG_LOG( SG_FLIGHT, SG_ALERT, "routine (coming up later in the code) will core dump.");
 259         SG_LOG( SG_FLIGHT, SG_ALERT, "Halting the sim now, and hoping a solution will present itself soon!");
 260         exit(-1);
 261     }
 262
 263     init_gear();
 264
 265     // Set initial fuel levels if provided.
 266     for (unsigned int i = 0; i < Propulsion->GetNumTanks(); i++) {
 267       double d;
 268       SGPropertyNode * node = fgGetNode("/consumables/fuel/tank", i, true);
 269       FGTank* tank = Propulsion->GetTank(i);
 270
 271       d = node->getNode( "density-ppg", true )->getDoubleValue();
 272       if( d > 0.0 ) {
 273         tank->SetDensity( d );
 274       } else {
 275         node->getNode( "density-ppg", true )->setDoubleValue( SG_MAX2<double>(tank->GetDensity(), 0.1) );
 276       }
 277
 278       d = node->getNode( "level-lbs", true )->getDoubleValue();
 279       if( d > 0.0 ) {
 280         tank->SetContents( d );
 281       } else {
 282         node->getNode( "level-lbs", true )->setDoubleValue( tank->GetContents() );
 283       }
 284       /* Capacity is read-only in FGTank and can't be overwritten from FlightGear */
 285       node->getNode("capacity-gal_us", true )->setDoubleValue( tank->GetCapacityGallons() );
 286     }
 287     Propulsion->SetFuelFreeze((fgGetNode("/sim/freeze/fuel",true))->getBoolValue());
 288
 289     fgSetDouble("/fdm/trim/pitch-trim", FCS->GetPitchTrimCmd());
 290     fgSetDouble("/fdm/trim/throttle",   FCS->GetThrottleCmd(0));
 291     fgSetDouble("/fdm/trim/aileron",    FCS->GetDaCmd());
 292     fgSetDouble("/fdm/trim/rudder",     FCS->GetDrCmd());
 293
 294     startup_trim = fgGetNode("/sim/presets/trim", true);
 295
 296     trimmed = fgGetNode("/fdm/trim/trimmed", true);
 297     trimmed->setBoolValue(false);
 298
 299     pitch_trim = fgGetNode("/fdm/trim/pitch-trim", true );
 300     throttle_trim = fgGetNode("/fdm/trim/throttle", true );
 301     aileron_trim = fgGetNode("/fdm/trim/aileron", true );
 302     rudder_trim = fgGetNode("/fdm/trim/rudder", true );
 303
 304     stall_warning = fgGetNode("/sim/alarms/stall-warning",true);
 305     stall_warning->setDoubleValue(0);
 306
 307
 308     flap_pos_pct=fgGetNode("/surface-positions/flap-pos-norm",true);
 309     elevator_pos_pct=fgGetNode("/surface-positions/elevator-pos-norm",true);
 310     left_aileron_pos_pct
 311         =fgGetNode("/surface-positions/left-aileron-pos-norm",true);
 312     right_aileron_pos_pct
 313         =fgGetNode("/surface-positions/right-aileron-pos-norm",true);
 314     rudder_pos_pct=fgGetNode("/surface-positions/rudder-pos-norm",true);
 315     speedbrake_pos_pct
 316         =fgGetNode("/surface-positions/speedbrake-pos-norm",true);
 317     spoilers_pos_pct=fgGetNode("/surface-positions/spoilers-pos-norm",true);
 318     tailhook_pos_pct=fgGetNode("/gear/tailhook/position-norm",true);
 319     wing_fold_pos_pct=fgGetNode("surface-positions/wing-fold-pos-norm",true);
 320
 321     elevator_pos_pct->setDoubleValue(0);
 322     left_aileron_pos_pct->setDoubleValue(0);
 323     right_aileron_pos_pct->setDoubleValue(0);
 324     rudder_pos_pct->setDoubleValue(0);
 325     flap_pos_pct->setDoubleValue(0);
 326     speedbrake_pos_pct->setDoubleValue(0);
 327     spoilers_pos_pct->setDoubleValue(0);
 328
 329     ab_brake_engaged = fgGetNode("/autopilot/autobrake/engaged", true);
 330     ab_brake_left_pct = fgGetNode("/autopilot/autobrake/brake-left-output", true);
 331     ab_brake_right_pct = fgGetNode("/autopilot/autobrake/brake-right-output", true);
 332
 333     altitude = fgGetNode("/position/altitude-ft");
 334     temperature = fgGetNode("/environment/temperature-degc",true);
 335     pressure = fgGetNode("/environment/pressure-inhg",true);
 336     pressureSL = fgGetNode("/environment/pressure-sea-level-inhg",true);
 337     ground_wind = fgGetNode("/environment/config/boundary/entry[0]/wind-speed-kt",true);
 338     turbulence_gain = fgGetNode("/environment/turbulence/magnitude-norm",true);
 339     turbulence_rate = fgGetNode("/environment/turbulence/rate-hz",true);
 340     turbulence_model = fgGetNode("/environment/params/jsbsim-turbulence-model",true);
 341
 342     wind_from_north= fgGetNode("/environment/wind-from-north-fps",true);
 343     wind_from_east = fgGetNode("/environment/wind-from-east-fps" ,true);
 344     wind_from_down = fgGetNode("/environment/wind-from-down-fps" ,true);
 345
 346     slaved = fgGetNode("/sim/slaved/enabled", true);
 347
 348     for (unsigned int i = 0; i < Propulsion->GetNumEngines(); i++) {
 349       SGPropertyNode * node = fgGetNode("engines/engine", i, true);
 350       Propulsion->GetEngine(i)->GetThruster()->SetRPM(node->getDoubleValue("rpm") /
 351                      Propulsion->GetEngine(i)->GetThruster()->GetGearRatio());
 352     }
 353
 354     hook_root_struct = FGColumnVector3(
 355         fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-offset-x-in", 196),
 356         fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-offset-y-in", 0),
 357         fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-offset-z-in", -16));
 358     last_hook_tip[0] = 0; last_hook_tip[1] = 0; last_hook_tip[2] = 0;
 359     last_hook_root[0] = 0; last_hook_root[1] = 0; last_hook_root[2] = 0;
 360
 361     crashed = false;
 362 }
 363
 364 /******************************************************************************/
 365 FGJSBsim::~FGJSBsim(void)
 366 {
 367   delete fdmex;
 368   delete PropertyManager;
 369 }
 370
 371 /******************************************************************************/
 372
 373 // Initialize the JSBsim flight model, dt is the time increment for
 374 // each subsequent iteration through the EOM
 375
 376 void FGJSBsim::init()
 377 {
 378     SG_LOG( SG_FLIGHT, SG_INFO, "Starting and initializing JSBsim" );
 379
 380     // Explicitly call the superclass's
 381     // init method first.
 382
 383     if (fgGetBool("/environment/params/control-fdm-atmosphere")) {
 384       Atmosphere->SetTemperature(temperature->getDoubleValue(), get_Altitude(), FGAtmosphere::eCelsius);
 385       Atmosphere->SetPressureSL(FGAtmosphere::eInchesHg, pressureSL->getDoubleValue());
 386       // initialize to no turbulence, these values get set in the update loop
 387       Winds->SetTurbType(FGWinds::ttNone);
 388       Winds->SetTurbGain(0.0);
 389       Winds->SetTurbRate(0.0);
 390       Winds->SetWindspeed20ft(0.0);
 391       Winds->SetProbabilityOfExceedence(0.0);
 392     }
 393
 394     fgic->SetWindNEDFpsIC(0.0, 0.0, 0.0);
 395
 396     SG_LOG(SG_FLIGHT,SG_INFO,"T,p,rho: " << Atmosphere->GetTemperature()
 397      << ", " << Atmosphere->GetPressure()
 398      << ", " << Atmosphere->GetDensity() );
 399
 400     FCS->SetDfPos( ofNorm, globals->get_controls()->get_flaps() );
 401
 402     needTrim = startup_trim->getBoolValue();
 403     common_init();
 404
 405     copy_to_JSBsim();
 406     fdmex->RunIC();     //loop JSBSim once w/o integrating
 407     if (fgGetBool("/sim/presets/running")) {
 408       Propulsion->InitRunning(-1);
 409       for (unsigned int i = 0; i < Propulsion->GetNumEngines(); i++) {
 410         FGPiston* eng = (FGPiston*)Propulsion->GetEngine(i);
 411         globals->get_controls()->set_magnetos(i, eng->GetMagnetos());
 412         globals->get_controls()->set_mixture(i, FCS->GetMixtureCmd(i));
 413       }
 414     }
 415
 416     if ( needTrim ) {
 417       const FGLocation& cart = fgic->GetPosition();
 418       double cart_pos[3], contact[3], d[3], vel[3], agl;
 419       update_ground_cache(cart, cart_pos, 0.01);
 420
 421       get_agl_ft(fdmex->GetSimTime(), cart_pos, SG_METER_TO_FEET*2, contact,
 422                  d, vel, d, &agl);
 423       double terrain_alt = sqrt(contact[0]*contact[0] + contact[1]*contact[1]
 424                                 + contact[2]*contact[2]) - cart.GetSeaLevelRadius();
 425
 426       SG_LOG(SG_FLIGHT, SG_INFO, "Ready to trim, terrain elevation is: "
 427                                  << terrain_alt );
 428
 429       if (fgGetBool("/sim/presets/onground")) {
 430         FGColumnVector3 gndVelNED = cart.GetTec2l()
 431                                   * FGColumnVector3(vel[0], vel[1], vel[2]);
 432         fgic->SetVNorthFpsIC(gndVelNED(1));
 433         fgic->SetVEastFpsIC(gndVelNED(2));
 434         fgic->SetVDownFpsIC(gndVelNED(3));
 435       }
 436       do_trim();
 437       needTrim = false;
 438     }
 439
 440     copy_from_JSBsim(); //update the bus
 441
 442     SG_LOG( SG_FLIGHT, SG_INFO, "  Initialized JSBSim with:" );
 443
 444     switch(fgic->GetSpeedSet()) {
 445     case setned:
 446         SG_LOG(SG_FLIGHT,SG_INFO, "  Vn,Ve,Vd= "
 447                << Propagate->GetVel(FGJSBBase::eNorth) << ", "
 448                << Propagate->GetVel(FGJSBBase::eEast) << ", "
 449                << Propagate->GetVel(FGJSBBase::eDown) << " ft/s");
 450     break;
 451     case setuvw:
 452         SG_LOG(SG_FLIGHT,SG_INFO, "  U,V,W= "
 453                << Propagate->GetUVW(1) << ", "
 454                << Propagate->GetUVW(2) << ", "
 455                << Propagate->GetUVW(3) << " ft/s");
 456     break;
 457     case setmach:
 458         SG_LOG(SG_FLIGHT,SG_INFO, "  Mach: "
 459                << Auxiliary->GetMach() );
 460     break;
 461     case setvc:
 462     default:
 463         SG_LOG(SG_FLIGHT,SG_INFO, "  Indicated Airspeed: "
 464                << Auxiliary->GetVcalibratedKTS() << " knots" );
 465     break;
 466     }
 467
 468     stall_warning->setDoubleValue(0);
 469
 470     SG_LOG( SG_FLIGHT, SG_INFO, "  Bank Angle: "
 471             << Propagate->GetEuler(FGJSBBase::ePhi)*RADTODEG << " deg" );
 472     SG_LOG( SG_FLIGHT, SG_INFO, "  Pitch Angle: "
 473             << Propagate->GetEuler(FGJSBBase::eTht)*RADTODEG << " deg" );
 474     SG_LOG( SG_FLIGHT, SG_INFO, "  True Heading: "
 475             << Propagate->GetEuler(FGJSBBase::ePsi)*RADTODEG << " deg" );
 476     SG_LOG( SG_FLIGHT, SG_INFO, "  Latitude: "
 477             << Propagate->GetLocation().GetLatitudeDeg() << " deg" );
 478     SG_LOG( SG_FLIGHT, SG_INFO, "  Longitude: "
 479             << Propagate->GetLocation().GetLongitudeDeg() << " deg" );
 480     SG_LOG( SG_FLIGHT, SG_INFO, "  Altitude: "
 481             << Propagate->GetAltitudeASL() << " feet" );
 482     SG_LOG( SG_FLIGHT, SG_INFO, "  loaded initial conditions" );
 483
 484     SG_LOG( SG_FLIGHT, SG_INFO, "  set dt" );
 485
 486     SG_LOG( SG_FLIGHT, SG_INFO, "Finished initializing JSBSim" );
 487
 488     SG_LOG( SG_FLIGHT, SG_INFO, "FGControls::get_gear_down()= " <<
 489                                   globals->get_controls()->get_gear_down() );
 490 }
 491
 492 /******************************************************************************/
 493
 494 void FGJSBsim::unbind()
 495 {
 496   fdmex->Unbind();
 497   FGInterface::unbind();
 498 }
 499
 500 /******************************************************************************/
 501
 502 // Run an iteration of the EOM (equations of motion)
 503
 504 void FGJSBsim::update( double dt )
 505 {
 506     if(crashed) {
 507       if(!fgGetBool("/sim/crashed"))
 508         fgSetBool("/sim/crashed", true);
 509       return;
 510     }
 511
 512     if (is_suspended())
 513       return;
 514
 515     int multiloop = _calc_multiloop(dt);
 516     FGLocation cart = Auxiliary->GetLocationVRP();
 517     double cart_pos[3];
 518
 519     update_ground_cache(cart, cart_pos, dt);
 520
 521     copy_to_JSBsim();
 522
 523     trimmed->setBoolValue(false);
 524
 525     for ( int i=0; i < multiloop; i++ ) {
 526       fdmex->Run();
 527       update_external_forces(fdmex->GetSimTime() + i * fdmex->GetDeltaT());
 528     }
 529
 530     FGJSBBase::Message* msg;
 531     while ((msg = fdmex->ProcessNextMessage()) != NULL) {
 532 //      msg = fdmex->ProcessNextMessage();
 533       switch (msg->type) {
 534       case FGJSBBase::Message::eText:
 535         if (msg->text == "Crash Detected: Simulation FREEZE.")
 536           crashed = true;
 537         SG_LOG( SG_FLIGHT, SG_INFO, msg->messageId << ": " << msg->text );
 538         break;
 539       case FGJSBBase::Message::eBool:
 540         SG_LOG( SG_FLIGHT, SG_INFO, msg->messageId << ": " << msg->text << " " << msg->bVal );
 541         break;
 542       case FGJSBBase::Message::eInteger:
 543         SG_LOG( SG_FLIGHT, SG_INFO, msg->messageId << ": " << msg->text << " " << msg->iVal );
 544         break;
 545       case FGJSBBase::Message::eDouble:
 546         SG_LOG( SG_FLIGHT, SG_INFO, msg->messageId << ": " << msg->text << " " << msg->dVal );
 547         break;
 548       default:
 549         SG_LOG( SG_FLIGHT, SG_INFO, "Unrecognized message type." );
 550         break;
 551       }
 552     }
 553
 554     // translate JSBsim back to FG structure so that the
 555     // autopilot (and the rest of the sim can use the updated values
 556     copy_from_JSBsim();
 557 }
 558
 559 /******************************************************************************/
 560
 561 void FGJSBsim::suspend()
 562 {
 563   fdmex->Hold();
 564   SGSubsystem::suspend();
 565 }
 566
 567 /******************************************************************************/
 568
 569 void FGJSBsim::resume()
 570 {
 571   fdmex->Resume();
 572   SGSubsystem::resume();
 573 }
 574
 575 /******************************************************************************/
 576
 577 // Convert from the FGInterface struct to the JSBsim generic_ struct
 578
 579 bool FGJSBsim::copy_to_JSBsim()
 580 {
 581     unsigned int i;
 582
 583     // copy control positions into the JSBsim structure
 584
 585     FCS->SetDaCmd( globals->get_controls()->get_aileron());
 586     FCS->SetRollTrimCmd( globals->get_controls()->get_aileron_trim() );
 587     FCS->SetDeCmd( globals->get_controls()->get_elevator());
 588     FCS->SetPitchTrimCmd( globals->get_controls()->get_elevator_trim() );
 589     FCS->SetDrCmd( -globals->get_controls()->get_rudder() );
 590     FCS->SetYawTrimCmd( -globals->get_controls()->get_rudder_trim() );
 591     FCS->SetDsCmd( globals->get_controls()->get_rudder() );
 592     FCS->SetDfCmd( globals->get_controls()->get_flaps() );
 593     FCS->SetDsbCmd( globals->get_controls()->get_speedbrake() );
 594     FCS->SetDspCmd( globals->get_controls()->get_spoilers() );
 595
 596         // Parking brake sets minimum braking
 597         // level for mains.
 598     double parking_brake = globals->get_controls()->get_brake_parking();
 599     double left_brake = globals->get_controls()->get_brake_left();
 600     double right_brake = globals->get_controls()->get_brake_right();
 601
 602     if (ab_brake_engaged->getBoolValue()) {
 603       left_brake = ab_brake_left_pct->getDoubleValue();
 604       right_brake = ab_brake_right_pct->getDoubleValue();
 605     }
 606
 607     FCS->SetLBrake(FMAX(left_brake, parking_brake));
 608     FCS->SetRBrake(FMAX(right_brake, parking_brake));
 609
 610
 611     FCS->SetCBrake( 0.0 );
 612     // FCS->SetCBrake( globals->get_controls()->get_brake(2) );
 613
 614     FCS->SetGearCmd( globals->get_controls()->get_gear_down());
 615     for (i = 0; i < Propulsion->GetNumEngines(); i++) {
 616       SGPropertyNode * node = fgGetNode("engines/engine", i, true);
 617
 618       FCS->SetThrottleCmd(i, globals->get_controls()->get_throttle(i));
 619       FCS->SetMixtureCmd(i, globals->get_controls()->get_mixture(i));
 620       FCS->SetPropAdvanceCmd(i, globals->get_controls()->get_prop_advance(i));
 621       FCS->SetFeatherCmd(i, globals->get_controls()->get_feather(i));
 622
 623       switch (Propulsion->GetEngine(i)->GetType()) {
 624       case FGEngine::etPiston:
 625         { // FGPiston code block
 626         FGPiston* eng = (FGPiston*)Propulsion->GetEngine(i);
 627         eng->SetMagnetos( globals->get_controls()->get_magnetos(i) );
 628         break;
 629         } // end FGPiston code block
 630       case FGEngine::etTurbine:
 631         { // FGTurbine code block
 632         FGTurbine* eng = (FGTurbine*)Propulsion->GetEngine(i);
 633         eng->SetAugmentation( globals->get_controls()->get_augmentation(i) );
 634         eng->SetReverse( globals->get_controls()->get_reverser(i) );
 635         //eng->SetInjection( globals->get_controls()->get_water_injection(i) );
 636         eng->SetCutoff( globals->get_controls()->get_cutoff(i) );
 637         eng->SetIgnition( globals->get_controls()->get_ignition(i) );
 638         break;
 639         } // end FGTurbine code block
 640       case FGEngine::etRocket:
 641         { // FGRocket code block
 642 //        FGRocket* eng = (FGRocket*)Propulsion->GetEngine(i);
 643         break;
 644         } // end FGRocket code block
 645       case FGEngine::etTurboprop:
 646         { // FGTurboProp code block
 647         FGTurboProp* eng = (FGTurboProp*)Propulsion->GetEngine(i);
 648         eng->SetReverse( globals->get_controls()->get_reverser(i) );
 649         eng->SetCutoff( globals->get_controls()->get_cutoff(i) );
 650         eng->SetIgnition( globals->get_controls()->get_ignition(i) );
 651
 652         eng->SetGeneratorPower( globals->get_controls()->get_generator_breaker(i) );
 653         eng->SetCondition( globals->get_controls()->get_condition(i) );
 654         break;
 655         } // end FGTurboProp code block
 656       default:
 657         break;
 658       }
 659
 660       { // FGEngine code block
 661       FGEngine* eng = Propulsion->GetEngine(i);
 662
 663       eng->SetStarter( globals->get_controls()->get_starter(i) );
 664       eng->SetRunning( node->getBoolValue("running") );
 665       } // end FGEngine code block
 666     }
 667
 668     Atmosphere->SetTemperature(temperature->getDoubleValue(), get_Altitude(), FGAtmosphere::eCelsius);
 669     Atmosphere->SetPressureSL(FGAtmosphere::eInchesHg, pressureSL->getDoubleValue());
 670
 671     Winds->SetTurbType((FGWinds::tType)TURBULENCE_TYPE_NAMES[turbulence_model->getStringValue()]);
 672     switch( Winds->GetTurbType() ) {
 673         case FGWinds::ttStandard:
 674         case FGWinds::ttCulp: {
 675             double tmp = turbulence_gain->getDoubleValue();
 676             Winds->SetTurbGain(tmp * tmp * 100.0);
 677             Winds->SetTurbRate(turbulence_rate->getDoubleValue());
 678             break;
 679         }
 680         case FGWinds::ttMilspec:
 681         case FGWinds::ttTustin: {
 682             // milspec turbulence: 3=light, 4=moderate, 6=severe turbulence
 683             // turbulence_gain normalized: 0: none, 1/3: light, 2/3: moderate, 3/3: severe
 684             double tmp = turbulence_gain->getDoubleValue();
 685             Winds->SetProbabilityOfExceedence(
 686               SGMiscd::roundToInt(TurbulenceSeverityTable.GetValue( tmp ) )
 687             );
 688             Winds->SetWindspeed20ft(ground_wind->getDoubleValue());
 689             break;
 690         }
 691
 692         default:
 693             break;
 694     }
 695
 696     Winds->SetWindNED( -wind_from_north->getDoubleValue(),
 697                        -wind_from_east->getDoubleValue(),
 698                        -wind_from_down->getDoubleValue() );
 699 //    SG_LOG(SG_FLIGHT,SG_INFO, "Wind NED: "
 700 //                  << get_V_north_airmass() << ", "
 701 //                  << get_V_east_airmass()  << ", "
 702 //                  << get_V_down_airmass() );
 703
 704     for (i = 0; i < Propulsion->GetNumTanks(); i++) {
 705       SGPropertyNode * node = fgGetNode("/consumables/fuel/tank", i, true);
 706       FGTank * tank = Propulsion->GetTank(i);
 707       double fuelDensity = node->getDoubleValue("density-ppg");
 708
 709       if (fuelDensity < 0.1)
 710         fuelDensity = 6.0; // Use average fuel value
 711
 712       tank->SetDensity(fuelDensity);
 713       tank->SetContents(node->getDoubleValue("level-lbs"));
 714     }
 715
 716     Propulsion->SetFuelFreeze((fgGetNode("/sim/freeze/fuel",true))->getBoolValue());
 717     fdmex->SetChild(slaved->getBoolValue());
 718
 719     return true;
 720 }
 721
 722 /******************************************************************************/
 723
 724 // Convert from the JSBsim generic_ struct to the FGInterface struct
 725
 726 bool FGJSBsim::copy_from_JSBsim()
 727 {
 728     unsigned int i, j;
 729 /*
 730     _set_Inertias( MassBalance->GetMass(),
 731                    MassBalance->GetIxx(),
 732                    MassBalance->GetIyy(),
 733                    MassBalance->GetIzz(),
 734                    MassBalance->GetIxz() );
 735 */
 736     _set_CG_Position( MassBalance->GetXYZcg(1),
 737                       MassBalance->GetXYZcg(2),
 738                       MassBalance->GetXYZcg(3) );
 739
 740     _set_Accels_Body( Accelerations->GetBodyAccel(1),
 741                       Accelerations->GetBodyAccel(2),
 742                       Accelerations->GetBodyAccel(3) );
 743
 744     _set_Accels_CG_Body_N ( Auxiliary->GetNcg(1),
 745                             Auxiliary->GetNcg(2),
 746                             Auxiliary->GetNcg(3) );
 747
 748     _set_Accels_Pilot_Body( Auxiliary->GetPilotAccel(1),
 749                             Auxiliary->GetPilotAccel(2),
 750                             Auxiliary->GetPilotAccel(3) );
 751
 752     _set_Nlf( Auxiliary->GetNlf() );
 753
 754     // Velocities
 755
 756     _set_Velocities_Local( Propagate->GetVel(FGJSBBase::eNorth),
 757                            Propagate->GetVel(FGJSBBase::eEast),
 758                            Propagate->GetVel(FGJSBBase::eDown) );
 759
 760     _set_Velocities_Body( Propagate->GetUVW(1),
 761                           Propagate->GetUVW(2),
 762                           Propagate->GetUVW(3) );
 763
 764     // Make the HUD work ...
 765     _set_Velocities_Ground( Propagate->GetVel(FGJSBBase::eNorth),
 766                             Propagate->GetVel(FGJSBBase::eEast),
 767                             -Propagate->GetVel(FGJSBBase::eDown) );
 768
 769     _set_V_rel_wind( Auxiliary->GetVt() );
 770
 771     _set_V_equiv_kts( Auxiliary->GetVequivalentKTS() );
 772
 773     _set_V_calibrated_kts( Auxiliary->GetVcalibratedKTS() );
 774
 775     _set_V_ground_speed( Auxiliary->GetVground() );
 776
 777     _set_Omega_Body( Propagate->GetPQR(FGJSBBase::eP),
 778                      Propagate->GetPQR(FGJSBBase::eQ),
 779                      Propagate->GetPQR(FGJSBBase::eR) );
 780
 781     _set_Euler_Rates( Auxiliary->GetEulerRates(FGJSBBase::ePhi),
 782                       Auxiliary->GetEulerRates(FGJSBBase::eTht),
 783                       Auxiliary->GetEulerRates(FGJSBBase::ePsi) );
 784
 785     _set_Mach_number( Auxiliary->GetMach() );
 786
 787     // Positions of Visual Reference Point
 788     FGLocation l = Auxiliary->GetLocationVRP();
 789     _updatePosition(SGGeoc::fromRadFt( l.GetLongitude(), l.GetLatitude(),
 790                                        l.GetRadius() ));
 791
 792     _set_Altitude_AGL( Propagate->GetDistanceAGL() );
 793     {
 794       double loc_cart[3] = { l(FGJSBBase::eX), l(FGJSBBase::eY), l(FGJSBBase::eZ) };
 795       double contact[3], d[3], sd, t;
 796       is_valid_m(&t, d, &sd);
 797       get_agl_ft(t, loc_cart, SG_METER_TO_FEET*2, contact, d, d, d, &sd);
 798       double rwrad
 799         = FGColumnVector3( contact[0], contact[1], contact[2] ).Magnitude();
 800       _set_Runway_altitude( rwrad - get_Sea_level_radius() );
 801     }
 802
 803     _set_Euler_Angles( Propagate->GetEuler(FGJSBBase::ePhi),
 804                        Propagate->GetEuler(FGJSBBase::eTht),
 805                        Propagate->GetEuler(FGJSBBase::ePsi) );
 806
 807     _set_Alpha( Auxiliary->Getalpha() );
 808     _set_Beta( Auxiliary->Getbeta() );
 809
 810
 811     _set_Gamma_vert_rad( Auxiliary->GetGamma() );
 812
 813     _set_Earth_position_angle( Propagate->GetEarthPositionAngle() );
 814
 815     _set_Climb_Rate( Propagate->Gethdot() );
 816
 817     const FGMatrix33& Tl2b = Propagate->GetTl2b();
 818     for ( i = 1; i <= 3; i++ ) {
 819         for ( j = 1; j <= 3; j++ ) {
 820             _set_T_Local_to_Body( i, j, Tl2b(i,j) );
 821         }
 822     }
 823
 824     // Copy the engine values from JSBSim.
 825     for ( i=0; i < Propulsion->GetNumEngines(); i++ ) {
 826       SGPropertyNode * node = fgGetNode("engines/engine", i, true);
 827       SGPropertyNode * tnode = node->getChild("thruster", 0, true);
 828       FGThruster * thruster = Propulsion->GetEngine(i)->GetThruster();
 829
 830       switch (Propulsion->GetEngine(i)->GetType()) {
 831       case FGEngine::etPiston:
 832         { // FGPiston code block
 833         FGPiston* eng = (FGPiston*)Propulsion->GetEngine(i);
 834         node->setDoubleValue("egt-degf", eng->getExhaustGasTemp_degF());
 835         node->setDoubleValue("oil-temperature-degf", eng->getOilTemp_degF());
 836         node->setDoubleValue("oil-pressure-psi", eng->getOilPressure_psi());
 837         node->setDoubleValue("mp-osi", eng->getManifoldPressure_inHg());
 838         // NOTE: mp-osi is not in ounces per square inch.
 839         // This error is left for reasons of backwards compatibility with
 840         // existing FlightGear sound and instrument configurations.
 841         node->setDoubleValue("mp-inhg", eng->getManifoldPressure_inHg());
 842         node->setDoubleValue("cht-degf", eng->getCylinderHeadTemp_degF());
 843         node->setDoubleValue("rpm", eng->getRPM());
 844         } // end FGPiston code block
 845         break;
 846       case FGEngine::etRocket:
 847         { // FGRocket code block
 848 //        FGRocket* eng = (FGRocket*)Propulsion->GetEngine(i);
 849         } // end FGRocket code block
 850         break;
 851       case FGEngine::etTurbine:
 852         { // FGTurbine code block
 853         FGTurbine* eng = (FGTurbine*)Propulsion->GetEngine(i);
 854         node->setDoubleValue("n1", eng->GetN1());
 855         node->setDoubleValue("n2", eng->GetN2());
 856         node->setDoubleValue("egt-degf", 32 + eng->GetEGT()*9/5);
 857         node->setBoolValue("augmentation", eng->GetAugmentation());
 858         node->setBoolValue("water-injection", eng->GetInjection());
 859         node->setBoolValue("ignition", eng->GetIgnition() != 0);
 860         node->setDoubleValue("nozzle-pos-norm", eng->GetNozzle());
 861         node->setDoubleValue("inlet-pos-norm", eng->GetInlet());
 862         node->setDoubleValue("oil-pressure-psi", eng->getOilPressure_psi());
 863         node->setBoolValue("reversed", eng->GetReversed());
 864         node->setBoolValue("cutoff", eng->GetCutoff());
 865         node->setDoubleValue("epr", eng->GetEPR());
 866         globals->get_controls()->set_reverser(i, eng->GetReversed() );
 867         globals->get_controls()->set_cutoff(i, eng->GetCutoff() );
 868         globals->get_controls()->set_water_injection(i, eng->GetInjection() );
 869         globals->get_controls()->set_augmentation(i, eng->GetAugmentation() );
 870         } // end FGTurbine code block
 871         break;
 872       case FGEngine::etTurboprop:
 873         { // FGTurboProp code block
 874         FGTurboProp* eng = (FGTurboProp*)Propulsion->GetEngine(i);
 875         node->setDoubleValue("n1", eng->GetN1());
 876         //node->setDoubleValue("n2", eng->GetN2());
 877         node->setDoubleValue("itt_degf", 32 + eng->GetITT()*9/5);
 878         node->setBoolValue("ignition", eng->GetIgnition() != 0);
 879         node->setDoubleValue("nozzle-pos-norm", eng->GetNozzle());
 880         node->setDoubleValue("inlet-pos-norm", eng->GetInlet());
 881         node->setDoubleValue("oil-pressure-psi", eng->getOilPressure_psi());
 882         node->setBoolValue("reversed", eng->GetReversed());
 883         node->setBoolValue("cutoff", eng->GetCutoff());
 884         node->setBoolValue("starting", eng->GetEngStarting());
 885         node->setBoolValue("generator-power", eng->GetGeneratorPower());
 886         node->setBoolValue("damaged", eng->GetCondition() != 0);
 887         node->setBoolValue("ielu-intervent", eng->GetIeluIntervent());
 888         node->setDoubleValue("oil-temperature-degf", eng->getOilTemp_degF());
 889 //        node->setBoolValue("onfire", eng->GetFire());
 890         globals->get_controls()->set_reverser(i, eng->GetReversed() );
 891         globals->get_controls()->set_cutoff(i, eng->GetCutoff() );
 892         } // end FGTurboProp code block
 893         break;
 894       case FGEngine::etElectric:
 895         { // FGElectric code block
 896         FGElectric* eng = (FGElectric*)Propulsion->GetEngine(i);
 897         node->setDoubleValue("rpm", eng->getRPM());
 898         } // end FGElectric code block
 899         break;
 900       case FGEngine::etUnknown:
 901         break;
 902       }
 903
 904       { // FGEngine code block
 905       FGEngine* eng = Propulsion->GetEngine(i);
 906       node->setDoubleValue("fuel-flow-gph", eng->getFuelFlow_gph());
 907       node->setDoubleValue("thrust_lb", thruster->GetThrust());
 908       node->setDoubleValue("fuel-flow_pph", eng->getFuelFlow_pph());
 909       node->setBoolValue("running", eng->GetRunning());
 910       node->setBoolValue("starter", eng->GetStarter());
 911       node->setBoolValue("cranking", eng->GetCranking());
 912       globals->get_controls()->set_starter(i, eng->GetStarter() );
 913       } // end FGEngine code block
 914
 915       switch (thruster->GetType()) {
 916       case FGThruster::ttNozzle:
 917         { // FGNozzle code block
 918 //        FGNozzle* noz = (FGNozzle*)thruster;
 919         } // end FGNozzle code block
 920         break;
 921       case FGThruster::ttPropeller:
 922         { // FGPropeller code block
 923         FGPropeller* prop = (FGPropeller*)thruster;
 924         tnode->setDoubleValue("rpm", thruster->GetRPM());
 925         tnode->setDoubleValue("pitch", prop->GetPitch());
 926         tnode->setDoubleValue("torque", prop->GetTorque());
 927         tnode->setBoolValue("feathered", prop->GetFeather());
 928         } // end FGPropeller code block
 929         break;
 930       case FGThruster::ttRotor:
 931         { // FGRotor code block
 932 //        FGRotor* rotor = (FGRotor*)thruster;
 933         } // end FGRotor code block
 934         break;
 935       case FGThruster::ttDirect:
 936         { // Direct code block
 937         } // end Direct code block
 938         break;
 939       }
 940
 941     }
 942
 943     // Copy the fuel levels from JSBSim if fuel
 944     // freeze not enabled.
 945     if ( ! Propulsion->GetFuelFreeze() ) {
 946       for (i = 0; i < Propulsion->GetNumTanks(); i++) {
 947         SGPropertyNode * node = fgGetNode("/consumables/fuel/tank", i, true);
 948         FGTank* tank = Propulsion->GetTank(i);
 949         double contents = tank->GetContents();
 950         double temp = tank->GetTemperature_degC();
 951         double fuelDensity = tank->GetDensity();
 952
 953         if (fuelDensity < 0.1)
 954           fuelDensity = 6.0; // Use average fuel value
 955
 956         node->setDoubleValue("density-ppg" , fuelDensity);
 957         node->setDoubleValue("level-lbs", contents);
 958         if (temp != -9999.0) node->setDoubleValue("temperature_degC", temp);
 959
 960         node->setDoubleValue("arm-in", tank->GetXYZ(FGJSBBase::eX ) );
 961       }
 962     }
 963
 964     update_gear();
 965
 966     stall_warning->setDoubleValue( Aerodynamics->GetStallWarn() );
 967
 968     elevator_pos_pct->setDoubleValue( FCS->GetDePos(ofNorm) );
 969     left_aileron_pos_pct->setDoubleValue( FCS->GetDaLPos(ofNorm) );
 970     right_aileron_pos_pct->setDoubleValue( FCS->GetDaRPos(ofNorm) );
 971     rudder_pos_pct->setDoubleValue( -1*FCS->GetDrPos(ofNorm) );
 972     flap_pos_pct->setDoubleValue( FCS->GetDfPos(ofNorm) );
 973     speedbrake_pos_pct->setDoubleValue( FCS->GetDsbPos(ofNorm) );
 974     spoilers_pos_pct->setDoubleValue( FCS->GetDspPos(ofNorm) );
 975     tailhook_pos_pct->setDoubleValue( FCS->GetTailhookPos() );
 976     wing_fold_pos_pct->setDoubleValue( FCS->GetWingFoldPos() );
 977
 978     // force a sim crashed if crashed (altitude AGL < 0)
 979     if (get_Altitude_AGL() < -100.0) {
 980          fdmex->SuspendIntegration();
 981          crashed = true;
 982     }
 983
 984     return true;
 985 }
 986
 987
 988 bool FGJSBsim::ToggleDataLogging(void)
 989 {
 990   // ToDo: handle this properly
 991   fdmex->DisableOutput();
 992   return false;
 993 }
 994
 995
 996 bool FGJSBsim::ToggleDataLogging(bool state)
 997 {
 998     if (state) {
 999       fdmex->EnableOutput();
1000       return true;
1001     } else {
1002       fdmex->DisableOutput();
1003       return false;
1004     }
1005 }
1006
1007
1008 //Positions
1009 void FGJSBsim::set_Latitude(double lat)
1010 {
1011   double alt = altitude->getDoubleValue();
1012   double sea_level_radius_meters, lat_geoc;
1013
1014   if ( alt < -9990 ) alt = 0.0;
1015
1016   SG_LOG(SG_FLIGHT,SG_INFO,"FGJSBsim::set_Latitude: " << lat );
1017   SG_LOG(SG_FLIGHT,SG_INFO," cur alt (ft) =  " << alt );
1018
1019   sgGeodToGeoc( lat, alt * SG_FEET_TO_METER,
1020                     &sea_level_radius_meters, &lat_geoc );
1021
1022   double sea_level_radius_ft = sea_level_radius_meters * SG_METER_TO_FEET;
1023   _set_Sea_level_radius( sea_level_radius_ft );
1024
1025   if (needTrim)
1026     fgic->SetLatitudeRadIC( lat_geoc );
1027   else
1028     Propagate->SetLatitude(lat_geoc);
1029
1030   FGInterface::set_Latitude(lat);
1031 }
1032
1033
1034 void FGJSBsim::set_Longitude(double lon)
1035 {
1036   SG_LOG(SG_FLIGHT,SG_INFO,"FGJSBsim::set_Longitude: " << lon );
1037
1038   if (needTrim)
1039     fgic->SetLongitudeRadIC(lon);
1040   else
1041     Propagate->SetLongitude(lon);
1042
1043   FGInterface::set_Longitude(lon);
1044 }
1045
1046 // Sets the altitude above sea level.
1047 void FGJSBsim::set_Altitude(double alt)
1048 {
1049   SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Altitude: " << alt );
1050
1051   if (needTrim) {
1052     FGLocation position = fgic->GetPosition();
1053
1054     position.SetPositionGeodetic(0.0, position.GetGeodLatitudeRad(), alt);
1055     fgic->SetAltitudeASLFtIC(position.GetAltitudeASL());
1056     fgic->SetLatitudeRadIC(position.GetLatitude());
1057   }
1058   else
1059     Propagate->SetAltitudeASL(alt);
1060
1061   FGInterface::set_Altitude(alt);
1062 }
1063
1064 void FGJSBsim::set_V_calibrated_kts(double vc)
1065 {
1066     SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_V_calibrated_kts: " <<  vc );
1067
1068   if (needTrim)
1069     fgic->SetVcalibratedKtsIC(vc);
1070   else {
1071     double p=pressure->getDoubleValue();
1072     double psl=fdmex->GetAtmosphere()->GetPressureSL();
1073     double rhosl=fdmex->GetAtmosphere()->GetDensitySL();
1074     double mach = FGJSBBase::MachFromVcalibrated(vc, p, psl, rhosl);
1075     double temp = 1.8*(temperature->getDoubleValue()+273.15);
1076     double soundSpeed = sqrt(1.4*1716.0*temp);
1077     FGColumnVector3 vUVW = Propagate->GetUVW();
1078     vUVW.Normalize();
1079     vUVW *= mach * soundSpeed;
1080     Propagate->SetUVW(1, vUVW(1));
1081     Propagate->SetUVW(2, vUVW(2));
1082     Propagate->SetUVW(3, vUVW(3));
1083   }
1084
1085   FGInterface::set_V_calibrated_kts(vc);
1086 }
1087
1088 void FGJSBsim::set_Mach_number(double mach)
1089 {
1090   SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Mach_number: " <<  mach );
1091
1092   if (needTrim)
1093     fgic->SetMachIC(mach);
1094   else {
1095     double temp = 1.8*(temperature->getDoubleValue()+273.15);
1096     double soundSpeed = sqrt(1.4*1716.0*temp);
1097     FGColumnVector3 vUVW = Propagate->GetUVW();
1098     vUVW.Normalize();
1099     vUVW *= mach * soundSpeed;
1100     Propagate->SetUVW(1, vUVW(1));
1101     Propagate->SetUVW(2, vUVW(2));
1102     Propagate->SetUVW(3, vUVW(3));
1103   }
1104
1105   FGInterface::set_Mach_number(mach);
1106 }
1107
1108 void FGJSBsim::set_Velocities_Local( double north, double east, double down )
1109 {
1110   SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Velocities_Local: "
1111      << north << ", " <<  east << ", " << down );
1112
1113   if (needTrim) {
1114     fgic->SetVNorthFpsIC(north);
1115     fgic->SetVEastFpsIC(east);
1116     fgic->SetVDownFpsIC(down);
1117   }
1118   else {
1119     FGColumnVector3 vNED(north, east, down);
1120     FGColumnVector3 vUVW = Propagate->GetTl2b() * vNED;
1121     Propagate->SetUVW(1, vUVW(1));
1122     Propagate->SetUVW(2, vUVW(2));
1123     Propagate->SetUVW(3, vUVW(3));
1124   }
1125
1126   FGInterface::set_Velocities_Local(north, east, down);
1127 }
1128
1129 void FGJSBsim::set_Velocities_Body( double u, double v, double w)
1130 {
1131   SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Velocities_Body: "
1132      << u << ", " <<  v << ", " <<  w );
1133
1134   if (needTrim) {
1135     fgic->SetUBodyFpsIC(u);
1136     fgic->SetVBodyFpsIC(v);
1137     fgic->SetWBodyFpsIC(w);
1138   }
1139   else {
1140     Propagate->SetUVW(1, u);
1141     Propagate->SetUVW(2, v);
1142     Propagate->SetUVW(3, w);
1143   }
1144
1145   FGInterface::set_Velocities_Body(u, v, w);
1146 }
1147
1148 //Euler angles
1149 void FGJSBsim::set_Euler_Angles( double phi, double theta, double psi )
1150 {
1151   SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Euler_Angles: "
1152      << phi << ", " << theta << ", " << psi );
1153
1154   if (needTrim) {
1155     fgic->SetThetaRadIC(theta);
1156     fgic->SetPhiRadIC(phi);
1157     fgic->SetPsiRadIC(psi);
1158   }
1159   else {
1160     FGQuaternion quat(phi, theta, psi);
1161     FGMatrix33 Tl2b = quat.GetT();
1162     FGMatrix33 Ti2b = Tl2b*Propagate->GetTi2l();
1163     FGQuaternion Qi = Ti2b.GetQuaternion();
1164     Propagate->SetInertialOrientation(Qi);
1165   }
1166
1167   FGInterface::set_Euler_Angles(phi, theta, psi);
1168 }
1169
1170 //Flight Path
1171 void FGJSBsim::set_Climb_Rate( double roc)
1172 {
1173   SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Climb_Rate: " << roc );
1174
1175   //since both climb rate and flight path angle are set in the FG
1176   //startup sequence, something is needed to keep one from cancelling
1177   //out the other.
1178   if( fabs(roc) > 1 && fabs(fgic->GetFlightPathAngleRadIC()) < 0.01 ) {
1179     if (needTrim)
1180       fgic->SetClimbRateFpsIC(roc);
1181     else {
1182       FGColumnVector3 vNED = Propagate->GetVel();
1183       vNED(FGJSBBase::eDown) = -roc;
1184       FGColumnVector3 vUVW = Propagate->GetTl2b() * vNED;
1185       Propagate->SetUVW(1, vUVW(1));
1186       Propagate->SetUVW(2, vUVW(2));
1187       Propagate->SetUVW(3, vUVW(3));
1188     }
1189
1190     FGInterface::set_Climb_Rate(roc);
1191   }
1192 }
1193
1194 void FGJSBsim::set_Gamma_vert_rad( double gamma)
1195 {
1196   SG_LOG(SG_FLIGHT,SG_INFO, "FGJSBsim::set_Gamma_vert_rad: " << gamma );
1197
1198   if( !(fabs(gamma) < 0.01 && fabs(fgic->GetClimbRateFpsIC()) > 1) ) {
1199     if (needTrim)
1200       fgic->SetFlightPathAngleRadIC(gamma);
1201     else {
1202       FGColumnVector3 vNED = Propagate->GetVel();
1203       double vt = vNED.Magnitude();
1204       vNED(FGJSBBase::eDown) = -vt * sin(gamma);
1205       FGColumnVector3 vUVW = Propagate->GetTl2b() * vNED;
1206       Propagate->SetUVW(1, vUVW(1));
1207       Propagate->SetUVW(2, vUVW(2));
1208       Propagate->SetUVW(3, vUVW(3));
1209     }
1210
1211     FGInterface::set_Gamma_vert_rad(gamma);
1212   }
1213 }
1214
1215 void FGJSBsim::init_gear(void )
1216 {
1217     FGGroundReactions* gr=fdmex->GetGroundReactions();
1218     int Ngear=GroundReactions->GetNumGearUnits();
1219     for (int i=0;i<Ngear;i++) {
1220       FGLGear *gear = gr->GetGearUnit(i);
1221       SGPropertyNode * node = fgGetNode("gear/gear", i, true);
1222       node->setDoubleValue("xoffset-in", gear->GetBodyLocation()(1) * 12);
1223       node->setDoubleValue("yoffset-in", gear->GetBodyLocation()(2) * 12);
1224       node->setDoubleValue("zoffset-in", gear->GetBodyLocation()(3) * 12);
1225       node->setBoolValue("wow", gear->GetWOW());
1226       node->setDoubleValue("rollspeed-ms", gear->GetWheelRollVel()*0.3043);
1227       node->setBoolValue("has-brake", gear->GetBrakeGroup() > 0);
1228       node->setDoubleValue("position-norm", gear->GetGearUnitPos());
1229 //    node->setDoubleValue("tire-pressure-norm", gear->GetTirePressure());
1230       node->setDoubleValue("compression-norm", gear->GetCompLen());
1231       node->setDoubleValue("compression-ft", gear->GetCompLen());
1232       if ( gear->GetSteerable() )
1233         node->setDoubleValue("steering-norm", gear->GetSteerNorm());
1234     }
1235 }
1236
1237 void FGJSBsim::update_gear(void)
1238 {
1239     FGGroundReactions* gr=fdmex->GetGroundReactions();
1240     int Ngear=GroundReactions->GetNumGearUnits();
1241     for (int i=0;i<Ngear;i++) {
1242       FGLGear *gear = gr->GetGearUnit(i);
1243       SGPropertyNode * node = fgGetNode("gear/gear", i, true);
1244       node->getChild("wow", 0, true)->setBoolValue( gear->GetWOW());
1245       node->getChild("rollspeed-ms", 0, true)->setDoubleValue(gear->GetWheelRollVel()*0.3043);
1246       node->getChild("position-norm", 0, true)->setDoubleValue(gear->GetGearUnitPos());
1247 //    gear->SetTirePressure(node->getDoubleValue("tire-pressure-norm"));
1248       node->setDoubleValue("compression-norm", gear->GetCompLen());
1249       node->setDoubleValue("compression-ft", gear->GetCompLen());
1250       if ( gear->GetSteerable() )
1251         node->setDoubleValue("steering-norm", gear->GetSteerNorm());
1252     }
1253 }
1254
1255 void FGJSBsim::do_trim(void)
1256 {
1257   FGTrim *fgtrim;
1258
1259   if ( fgGetBool("/sim/presets/onground") )
1260   {
1261     fgtrim = new FGTrim(fdmex,tGround);
1262   } else {
1263     fgtrim = new FGTrim(fdmex,tFull);
1264   }
1265
1266   if ( !fgtrim->DoTrim() ) {
1267     fgtrim->Report();
1268     fgtrim->TrimStats();
1269   } else {
1270     trimmed->setBoolValue(true);
1271   }
1272   delete fgtrim;
1273
1274   pitch_trim->setDoubleValue( FCS->GetPitchTrimCmd() );
1275   throttle_trim->setDoubleValue( FCS->GetThrottleCmd(0) );
1276   aileron_trim->setDoubleValue( FCS->GetDaCmd() );
1277   rudder_trim->setDoubleValue( -FCS->GetDrCmd() );
1278
1279   globals->get_controls()->set_elevator_trim(FCS->GetPitchTrimCmd());
1280   globals->get_controls()->set_elevator(FCS->GetDeCmd());
1281   for( unsigned i = 0; i < Propulsion->GetNumEngines(); i++ )
1282     globals->get_controls()->set_throttle(i, FCS->GetThrottleCmd(i));
1283
1284   globals->get_controls()->set_aileron(FCS->GetDaCmd());
1285   globals->get_controls()->set_rudder( -FCS->GetDrCmd());
1286
1287   SG_LOG( SG_FLIGHT, SG_INFO, "  Trim complete" );
1288 }
1289
1290 bool FGJSBsim::update_ground_cache(const FGLocation& cart, double* cart_pos,
1291                                    double dt)
1292 {
1293   // Compute the radius of the aircraft. That is the radius of a ball
1294   // where all gear units are in. At the moment it is at least 10ft ...
1295   double acrad = 10.0;
1296   int n_gears = GroundReactions->GetNumGearUnits();
1297   for (int i=0; i<n_gears; ++i) {
1298     FGColumnVector3 bl = GroundReactions->GetGearUnit(i)->GetBodyLocation();
1299     double r = bl.Magnitude();
1300     if (acrad < r)
1301       acrad = r;
1302   }
1303
1304   // Compute the potential movement of this aircraft and query for the
1305   // ground in this area.
1306   double groundCacheRadius = acrad + 2*dt*Propagate->GetUVW().Magnitude();
1307   cart_pos[0] = cart(1);
1308   cart_pos[1] = cart(2);
1309   cart_pos[2] = cart(3);
1310   double t0 = fdmex->GetSimTime();
1311   bool cache_ok = prepare_ground_cache_ft( t0, t0 + dt, cart_pos,
1312                                            groundCacheRadius );
1313   if (!cache_ok) {
1314     SG_LOG(SG_FLIGHT, SG_WARN,
1315            "FGInterface is being called without scenery below the aircraft!");
1316
1317     SG_LOG(SG_FLIGHT, SG_WARN, "altitude         = "
1318                       << fgic->GetAltitudeASLFtIC());
1319
1320     SG_LOG(SG_FLIGHT, SG_WARN, "sea level radius = "
1321                       << get_Sea_level_radius());
1322
1323     SG_LOG(SG_FLIGHT, SG_WARN, "latitude         = "
1324                       << fgic->GetLatitudeRadIC());
1325
1326     SG_LOG(SG_FLIGHT, SG_WARN, "longitude        = "
1327                       << fgic->GetLongitudeRadIC());
1328   }
1329
1330   return cache_ok;
1331 }
1332
1333 bool
1334 FGJSBsim::get_agl_ft(double t, const double pt[3], double alt_off,
1335                      double contact[3], double normal[3], double vel[3],
1336                      double angularVel[3], double *agl)
1337 {
1338   const simgear::BVHMaterial* material;
1339   simgear::BVHNode::Id id;
1340
1341   // don't check the return value and continue above scenery discontinuity
1342   // see http://osdir.com/ml/flightgear-sim/2014-04/msg00145.html
1343   FGInterface::get_agl_ft(t, pt, alt_off, contact, normal, vel,
1344                                angularVel, material, id);
1345
1346   SGGeod geodPt = SGGeod::fromCart(SG_FEET_TO_METER*SGVec3d(pt));
1347   SGQuatd hlToEc = SGQuatd::fromLonLat(geodPt);
1348   *agl = dot(hlToEc.rotate(SGVec3d(0, 0, 1)), SGVec3d(contact) - SGVec3d(pt));
1349
1350   static SGPropertyNode_ptr terrain = fgGetNode("/sim/fdm/surface", true);
1351
1352 #ifdef JSBSIM_USE_GROUNDREACTIONS
1353   bool terrain_active = (terrain->getIntValue("override-level", -1) > 0) ? false : true;
1354   terrain->setBoolValue("active", terrain_active);
1355   terrain->setBoolValue("valid", (material && terrain_active) ? true : false);
1356   if (terrain_active)
1357   {
1358     static bool material_valid = false;
1359     if (material) {
1360       GroundReactions->SetStaticFFactor((*material).get_friction_factor());
1361       GroundReactions->SetRollingFFactor((*material).get_rolling_friction()/0.02);
1362       // 1 Pascal = 0.00014503773800721815 lbs/in^2
1363       double pressure = (*material).get_load_resistance(); // N/m^2 (or Pascal)
1364       GroundReactions->SetMaximumForce(pressure*0.00014503773800721815);
1365
1366       GroundReactions->SetBumpiness((*material).get_bumpiness());
1367       GroundReactions->SetSolid((*material).get_solid());
1368       GroundReactions->SetPosition(pt);
1369       material_valid = true;
1370     } else {
1371        if (material_valid) {
1372          GroundReactions->resetValues();
1373          material_valid = false;
1374       }
1375     }
1376   }
1377 #else
1378   terrain->setBoolValue("valid", false);
1379 #endif
1380   return true;
1381 }
1382
1383 inline static double sqr(double x)
1384 {
1385     return x * x;
1386 }
1387
1388 static double angle_diff(double a, double b)
1389 {
1390     double diff = fabs(a - b);
1391     if (diff > 180) diff = 360 - diff;
1392
1393     return diff;
1394 }
1395
1396 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)
1397 {
1398     FGColumnVector3 tip(-hook_length * cos_fi_guess, 0, hook_length * sin_fi_guess);
1399     double dist = DotProduct(tip, ground_normal_body);
1400     if (fabs(dist + E) < 0.0001) {
1401         sin_fis[*points] = sin_fi_guess;
1402         cos_fis[*points] = cos_fi_guess;
1403         fis[*points] = atan2(sin_fi_guess, cos_fi_guess) * SG_RADIANS_TO_DEGREES;
1404         (*points)++;
1405     }
1406 }
1407
1408
1409 static void check_hook_solution(const FGColumnVector3& ground_normal_body, double E, double hook_length, double sin_fi_guess, double* sin_fis, double* cos_fis, double* fis, int* points)
1410 {
1411     if (sin_fi_guess >= -1 && sin_fi_guess <= 1) {
1412         double cos_fi_guess = sqrt(1 - sqr(sin_fi_guess));
1413         check_hook_solution(ground_normal_body, E, hook_length, sin_fi_guess, cos_fi_guess, sin_fis, cos_fis, fis, points);
1414         if (fabs(cos_fi_guess) > SG_EPSILON) {
1415             check_hook_solution(ground_normal_body, E, hook_length, sin_fi_guess, -cos_fi_guess, sin_fis, cos_fis, fis, points);
1416         }
1417     }
1418 }
1419
1420 void FGJSBsim::update_external_forces(double t_off)
1421 {
1422     const FGMatrix33& Tb2l = Propagate->GetTb2l();
1423     const FGMatrix33& Tl2b = Propagate->GetTl2b();
1424     const FGLocation& Location = Propagate->GetLocation();
1425     const FGMatrix33& Tec2l = Location.GetTec2l();
1426
1427     double hook_area[4][3];
1428
1429     FGColumnVector3 hook_root_body = MassBalance->StructuralToBody(hook_root_struct);
1430     FGColumnVector3 hook_root = Location.LocalToLocation(Tb2l *   hook_root_body);
1431     hook_area[1][0] = hook_root(1);
1432     hook_area[1][1] = hook_root(2);
1433     hook_area[1][2] = hook_root(3);
1434
1435     hook_length = fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-length-ft", 6.75);
1436     double fi_min = fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-pos-min-deg", -18);
1437     double fi_max = fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-pos-max-deg", 30);
1438     double fi = fgGetDouble("/fdm/jsbsim/systems/hook/tailhook-pos-norm") * (fi_max - fi_min) + fi_min;
1439     double cos_fi = cos(fi * SG_DEGREES_TO_RADIANS);
1440     double sin_fi = sin(fi * SG_DEGREES_TO_RADIANS);
1441
1442     FGColumnVector3 hook_tip_body = hook_root_body;
1443     hook_tip_body(1) -= hook_length * cos_fi;
1444     hook_tip_body(3) += hook_length * sin_fi;
1445
1446     double contact[3];
1447     double ground_normal[3];
1448     double ground_vel[3];
1449     double ground_angular_vel[3];
1450     double root_agl_ft;
1451
1452     if (!got_wire) {
1453         bool got = get_agl_ft(t_off, hook_area[1], 0, contact, ground_normal,
1454                               ground_vel, ground_angular_vel, &root_agl_ft);
1455         if (got && root_agl_ft > 0 && root_agl_ft < hook_length) {
1456             FGColumnVector3 ground_normal_body = Tl2b * (Tec2l * FGColumnVector3(ground_normal[0], ground_normal[1], ground_normal[2]));
1457             FGColumnVector3 contact_body = Tl2b * Location.LocationToLocal(FGColumnVector3(contact[0], contact[1], contact[2]));
1458             double D = -DotProduct(contact_body, ground_normal_body);
1459
1460             // check hook tip agl against same ground plane
1461             double hook_tip_agl_ft = DotProduct(hook_tip_body, ground_normal_body) + D;
1462             if (hook_tip_agl_ft < 0) {
1463
1464                 // hook tip: hx - l cos, hy, hz + l sin
1465                 // on ground:  - n0 l cos + n2 l sin + E = 0
1466
1467                 double E = D + DotProduct(hook_root_body, ground_normal_body);
1468
1469                 // substitue x = sin fi, cos fi = sqrt(1 - x * x)
1470                 // and rearrange to get a quadratic with coeffs:
1471                 double a = sqr(hook_length) * (sqr(ground_normal_body(1)) + sqr(ground_normal_body(3)));
1472                 double b = 2 * E * ground_normal_body(3) * hook_length;
1473                 double c = sqr(E) - sqr(ground_normal_body(1) * hook_length);
1474
1475                 double disc = sqr(b) - 4 * a * c;
1476                 if (disc >= 0) {
1477                     double delta = sqrt(disc) / (2 * a);
1478
1479                     // allow 4 solutions for safety, should never happen
1480                     double sin_fis[4];
1481                     double cos_fis[4];
1482                     double fis[4];
1483                     int points = 0;
1484
1485                     double sin_fi_guess = -b / (2 * a) - delta;
1486                     check_hook_solution(ground_normal_body, E, hook_length, sin_fi_guess, sin_fis, cos_fis, fis, &points);
1487                     check_hook_solution(ground_normal_body, E, hook_length, sin_fi_guess + 2 * delta, sin_fis, cos_fis, fis, &points);
1488
1489                     if (points == 2) {
1490                         double diff1 = angle_diff(fi, fis[0]);
1491                         double diff2 = angle_diff(fi, fis[1]);
1492                         int point = diff1 < diff2 ? 0 : 1;
1493                         fi = fis[point];
1494                         sin_fi = sin_fis[point];
1495                         cos_fi = cos_fis[point];
1496                         hook_tip_body(1) = hook_root_body(1) - hook_length * cos_fi;
1497                         hook_tip_body(3) = hook_root_body(3) + hook_length * sin_fi;
1498                     }
1499                 }
1500             }
1501         }
1502     } else {
1503         FGColumnVector3 hook_root_vel = Propagate->GetVel() + (Tb2l * (Propagate->GetPQR() *  hook_root_body));
1504         double wire_ends_ec[2][3];
1505         double wire_vel_ec[2][3];
1506         get_wire_ends_ft(t_off, wire_ends_ec, wire_vel_ec);
1507         FGColumnVector3 wire_vel_1 = Tec2l * FGColumnVector3(wire_vel_ec[0][0], wire_vel_ec[0][1], wire_vel_ec[0][2]);
1508         FGColumnVector3 wire_vel_2 = Tec2l * FGColumnVector3(wire_vel_ec[1][0], wire_vel_ec[1][1], wire_vel_ec[1][2]);
1509         FGColumnVector3 rel_vel = hook_root_vel - (wire_vel_1 + wire_vel_2) / 2;
1510         if (rel_vel.Magnitude() < 3) {
1511             got_wire = false;
1512             release_wire();
1513             fgSetDouble("/fdm/jsbsim/external_reactions/hook/magnitude", 0.0);
1514         } else {
1515             FGColumnVector3 wire_end1_body = Tl2b * Location.LocationToLocal(FGColumnVector3(wire_ends_ec[0][0], wire_ends_ec[0][1], wire_ends_ec[0][2])) - hook_root_body;
1516             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;
1517             FGColumnVector3 force_plane_normal = wire_end1_body * wire_end2_body;
1518             force_plane_normal.Normalize();
1519             cos_fi = DotProduct(force_plane_normal, FGColumnVector3(0, 0, 1));
1520             if (cos_fi < 0) cos_fi = -cos_fi;
1521             sin_fi = sqrt(1 - sqr(cos_fi));
1522             fi = atan2(sin_fi, cos_fi) * SG_RADIANS_TO_DEGREES;
1523
1524             fgSetDouble("/fdm/jsbsim/external_reactions/hook/x", -cos_fi);
1525             fgSetDouble("/fdm/jsbsim/external_reactions/hook/y", 0);
1526             fgSetDouble("/fdm/jsbsim/external_reactions/hook/z", sin_fi);
1527             fgSetDouble("/fdm/jsbsim/external_reactions/hook/magnitude", fgGetDouble("/fdm/jsbsim/systems/hook/force"));
1528         }
1529     }
1530
1531     FGColumnVector3 hook_tip = Location.LocalToLocation(Tb2l * hook_tip_body);
1532
1533     hook_area[0][0] = hook_tip(1);
1534     hook_area[0][1] = hook_tip(2);
1535     hook_area[0][2] = hook_tip(3);
1536
1537     if (!got_wire) {
1538         // The previous positions.
1539         hook_area[2][0] = last_hook_root[0];
1540         hook_area[2][1] = last_hook_root[1];
1541         hook_area[2][2] = last_hook_root[2];
1542         hook_area[3][0] = last_hook_tip[0];
1543         hook_area[3][1] = last_hook_tip[1];
1544         hook_area[3][2] = last_hook_tip[2];
1545
1546         // Check if we caught a wire.
1547         // Returns true if we caught one.
1548         if (caught_wire_ft(t_off, hook_area)) {
1549                 got_wire = true;
1550         }
1551     }
1552
1553     // save actual position as old position ...
1554     last_hook_tip[0] = hook_area[0][0];
1555     last_hook_tip[1] = hook_area[0][1];
1556     last_hook_tip[2] = hook_area[0][2];
1557     last_hook_root[0] = hook_area[1][0];
1558     last_hook_root[1] = hook_area[1][1];
1559     last_hook_root[2] = hook_area[1][2];
1560
1561     fgSetDouble("/fdm/jsbsim/systems/hook/tailhook-pos-deg", fi);
1562 }
1563