// Constructor
FGInterface::FGInterface() {
+ _setup();
+}
+
+FGInterface::FGInterface( double dt ) {
+
+ _setup();
+ delta_t = dt;
+ remainder = elapsed = multi_loop = 0;
+}
+
+// Destructor
+FGInterface::~FGInterface() {
+// unbind(); // FIXME: should be called explicitly
+}
+
+
+/**
+ * Set default values for the state of the FDM.
+ *
+ * This method is invoked by the constructors.
+ */
+void
+FGInterface::_setup ()
+{
init_vec( d_pilot_rp_body_v );
init_vec( d_cg_rp_body_v );
init_vec( f_body_total_v );
sin_latitude=cos_latitude=0;
sin_longitude=cos_longitude=0;
altitude_agl=0;
-}
-
-FGInterface::FGInterface( double dt ) {
- FGInterface();
-
- delta_t = dt;
- remainder = elapsed = multi_loop = 0;
-}
-
-// Destructor
-FGInterface::~FGInterface() {
-// unbind(); // FIXME: should be called explicitly
}
+/**
+ * Initialize the state of the FDM.
+ *
+ * Subclasses of FGInterface may do their own, additional initialization,
+ * but normally they should invoke this method explicitly first as
+ * FGInterface::init() to make sure the basic structures are set up
+ * properly.
+ */
void
FGInterface::init ()
{
+ SG_LOG(SG_FLIGHT, SG_INFO, "Start initializing FGInterface");
+
+ stamp();
+ set_remainder(0);
+
+ // Set initial position
+ SG_LOG(SG_FLIGHT, SG_INFO, "...initializing position...");
+ set_Longitude(fgGetDouble("/position/longitude-deg") * SGD_DEGREES_TO_RADIANS);
+ set_Latitude(fgGetDouble("/position/latitude-deg") * SGD_DEGREES_TO_RADIANS);
+ double ground_elev_m = scenery.cur_elev + 1;
+ double ground_elev_ft = ground_elev_m * METERS_TO_FEET;
+ if (fgGetBool("/sim/startup/onground") ||
+ fgGetDouble("/position/altitude-ft") < ground_elev_ft)
+ fgSetDouble("/position/altitude-ft", ground_elev_ft);
+ set_Altitude(fgGetDouble("/position/altitude-ft"));
+
+ // Set ground elevation
+ SG_LOG(SG_FLIGHT, SG_INFO,
+ "...initializing ground elevation to "
+ << ground_elev_ft << "ft...");
+ fgFDMSetGroundElevation("jsb", ground_elev_m);
+
+ // Set sea-level radius
+ SG_LOG(SG_FLIGHT, SG_INFO, "...initializing sea-level radius...");
+ double sea_level_radius_meters;
+ double lat_geoc;
+ sgGeodToGeoc(get_Latitude(), get_Altitude(),
+ &sea_level_radius_meters, &lat_geoc);
+ set_Sea_level_radius(sea_level_radius_meters * SG_METER_TO_FEET);
+
+ // Set initial velocities
+ SG_LOG(SG_FLIGHT, SG_INFO, "...initializing velocities...");
+ if (!fgHasNode("/sim/startup/speed-set")) {
+ set_V_calibrated_kts(0.0);
+ } else {
+ const string speedset = fgGetString("/sim/startup/speed-set");
+ if (speedset == "knots" || speedset == "KNOTS") {
+ set_V_calibrated_kts(fgGetDouble("/velocities/airspeed-kt"));
+ } else if (speedset == "mach" || speedset == "MACH") {
+ set_Mach_number(fgGetDouble("/velocities/mach"));
+ } else if (speedset == "UVW" || speedset == "uvw") {
+ set_Velocities_Wind_Body(fgGetDouble("/velocities/uBody-fps"),
+ fgGetDouble("/velocities/vBody-fps"),
+ fgGetDouble("/velocities/wBody-fps"));
+ } else if (speedset == "NED" || speedset == "ned") {
+ set_Velocities_Local(fgGetDouble("/velocities/speed-north-fps"),
+ fgGetDouble("/velocities/speed-east-fps"),
+ fgGetDouble("/velocities/speed-down-fps"));
+ } else {
+ SG_LOG(SG_FLIGHT, SG_ALERT,
+ "Unrecognized value for /sim/startup/speed-set: " << speedset);
+ set_V_calibrated_kts(0.0);
+ }
+ }
+
+ // Set initial Euler angles
+ SG_LOG(SG_FLIGHT, SG_INFO, "...initializing Euler angles...");
+ set_Euler_Angles
+ (fgGetDouble("/orientation/roll-deg") * SGD_DEGREES_TO_RADIANS,
+ fgGetDouble("/orientation/pitch-deg") * SGD_DEGREES_TO_RADIANS,
+ fgGetDouble("/orientation/heading-deg") * SGD_DEGREES_TO_RADIANS);
+
+ SG_LOG(SG_FLIGHT, SG_INFO, "End initializing FGInterface");
}
+
+/**
+ * Bind getters and setters to properties.
+ *
+ * The bind() method will be invoked after init(). Note that unlike
+ * the usual implementations of FGSubsystem::bind(), this method does
+ * not automatically pick up existing values for the properties at
+ * bind time; instead, all values are set explicitly in the init()
+ * method.
+ */
void
FGInterface::bind ()
{
- // Time management
+ // Time management (read-only)
fgTie("/fdm/time/delta_t", this,
- &(FGInterface::get_delta_t));
-
- // The following two can't be uncommented until we have support for
- // the "long" data type in the property manager
- /* fgTie("/fdm/time/elapsed", this,
- &(FGInterface::get_elapsed));
+ &FGInterface::get_delta_t); // read-only
+ fgTie("/fdm/time/elapsed", this,
+ &FGInterface::get_elapsed); // read-only
fgTie("/fdm/time/remainder", this,
- &(FGInterface::get_remainder); */
+ &FGInterface::get_remainder); // read-only
fgTie("/fdm/time/multi_loop", this,
- &(FGInterface::get_multi_loop));
+ &FGInterface::get_multi_loop); // read-only
// Aircraft position
- fgTie("/position/latitude", this,
- &(FGInterface::get_Latitude_deg),
- &(FGInterface::set_Latitude_deg));
- fgTie("/position/longitude", this,
- &(FGInterface::get_Longitude_deg),
- &(FGInterface::set_Longitude_deg));
- fgTie("/position/altitude", this,
- &(FGInterface::get_Altitude),
- &(FGInterface::set_Altitude));
- fgTie("/position/altitude-agl", this,
- &(FGInterface::get_Altitude_AGL)); // read-only
+ fgTie("/position/latitude-deg", this,
+ &FGInterface::get_Latitude_deg,
+ &FGInterface::set_Latitude_deg,
+ false);
+ fgTie("/position/longitude-deg", this,
+ &FGInterface::get_Longitude_deg,
+ &FGInterface::set_Longitude_deg,
+ false);
+ fgTie("/position/altitude-ft", this,
+ &FGInterface::get_Altitude,
+ &FGInterface::set_Altitude,
+ false);
+ fgTie("/position/altitude-agl-ft", this,
+ &FGInterface::get_Altitude_AGL); // read-only
// Orientation
- fgTie("/orientation/roll", this,
- &(FGInterface::get_Phi_deg),
- &(FGInterface::set_Phi_deg));
- fgTie("/orientation/pitch", this,
- &(FGInterface::get_Theta_deg),
- &(FGInterface::set_Theta_deg));
- fgTie("/orientation/heading", this,
- &(FGInterface::get_Psi_deg),
- &(FGInterface::set_Psi_deg));
+ fgTie("/orientation/roll-deg", this,
+ &FGInterface::get_Phi_deg,
+ &FGInterface::set_Phi_deg);
+ fgTie("/orientation/pitch-deg", this,
+ &FGInterface::get_Theta_deg,
+ &FGInterface::set_Theta_deg);
+ fgTie("/orientation/heading-deg", this,
+ &FGInterface::get_Psi_deg,
+ &FGInterface::set_Psi_deg);
// Calibrated airspeed
- fgTie("/velocities/airspeed", this,
- &(FGInterface::get_V_calibrated_kts),
- &(FGInterface::set_V_calibrated_kts));
+ fgTie("/velocities/airspeed-kt", this,
+ &FGInterface::get_V_calibrated_kts,
+ &FGInterface::set_V_calibrated_kts);
// Local velocities
- fgTie("/velocities/speed-north", this,
- &(FGInterface::get_V_north));
- fgTie("/velocities/speed-east", this,
- &(FGInterface::get_V_east),
- &(FGInterface::set_V_east));
- fgTie("/velocities/speed-down", this,
- &(FGInterface::get_V_down),
- &(FGInterface::set_V_down));
+ fgTie("/velocities/speed-north-fps", this,
+ &FGInterface::get_V_north,
+ &FGInterface::set_V_north);
+ fgTie("/velocities/speed-east-fps", this,
+ &FGInterface::get_V_east,
+ &FGInterface::set_V_east);
+ fgTie("/velocities/speed-down-fps", this,
+ &FGInterface::get_V_down,
+ &FGInterface::set_V_down);
// Relative wind
- fgTie("/velocities/uBody", this,
- &(FGInterface::get_uBody),
- &(FGInterface::set_uBody));
- fgTie("/velocities/vBody", this,
- &(FGInterface::get_vBody),
- &(FGInterface::set_vBody));
- fgTie("/velocities/wBody", this,
- &(FGInterface::get_wBody),
- &(FGInterface::set_wBody));
+ fgTie("/velocities/uBody-fps", this,
+ &FGInterface::get_uBody,
+ &FGInterface::set_uBody);
+ fgTie("/velocities/vBody-fps", this,
+ &FGInterface::get_vBody,
+ &FGInterface::set_vBody);
+ fgTie("/velocities/wBody-fps", this,
+ &FGInterface::get_wBody,
+ &FGInterface::set_wBody);
// Climb and slip (read-only)
- fgTie("/velocities/vertical-speed", this,
- &(FGInterface::get_Climb_Rate)); // read-only
- fgTie("/velocities/side-slip", this,
- &(FGInterface::get_Beta)); // read-only
+ fgTie("/velocities/vertical-speed-fps", this,
+ &FGInterface::get_Climb_Rate); // read-only
+ fgTie("/velocities/side-slip-rad", this,
+ &FGInterface::get_Beta); // read-only
}
+
+/**
+ * Unbind any properties bound to this FDM.
+ *
+ * This method allows the FDM to release properties so that a new
+ * FDM can bind them instead.
+ */
void
FGInterface::unbind ()
{
fgUntie("/fdm/time/elapsed");
fgUntie("/fdm/time/remainder");
fgUntie("/fdm/time/multi_loop");
- fgUntie("/position/latitude");
- fgUntie("/position/longitude");
- fgUntie("/position/altitude");
+ fgUntie("/position/latitude-deg");
+ fgUntie("/position/longitude-deg");
+ fgUntie("/position/altitude-ft");
fgUntie("/position/heading");
fgUntie("/position/pitch");
fgUntie("/position/roll");
- fgUntie("/velocities/airspeed");
- fgUntie("/velocities/speed-north");
- fgUntie("/velocities/speed-east");
- fgUntie("/velocities/speed-down");
- fgUntie("/velocities/uBody");
- fgUntie("/velocities/vBody");
- fgUntie("/velocities/wBody");
- fgUntie("/velocities/vertical-speed");
- fgUntie("/velocities/side-slip");
+ fgUntie("/velocities/airspeed-kt");
+ fgUntie("/velocities/speed-north-fps");
+ fgUntie("/velocities/speed-east-fps");
+ fgUntie("/velocities/speed-down-fps");
+ fgUntie("/velocities/uBody-fps");
+ fgUntie("/velocities/vBody-fps");
+ fgUntie("/velocities/wBody-fps");
+ fgUntie("/velocities/vertical-speed-fps");
+ fgUntie("/velocities/side-slip-rad");
}
+
+/**
+ * Update the state of the FDM (i.e. run the equations of motion).
+ */
void
FGInterface::update ()
{
void FGInterface::_updatePosition( double lat_geoc, double lon, double alt ) {
double lat_geod, tmp_alt, sl_radius1, sl_radius2, tmp_lat_geoc;
- sgGeocToGeod( lat_geoc, ( get_Sea_level_radius() + alt ) * FEET_TO_METER,
+ sgGeocToGeod( lat_geoc, ( get_Sea_level_radius() + alt ) * SG_FEET_TO_METER,
&lat_geod, &tmp_alt, &sl_radius1 );
- sgGeodToGeoc( lat_geod, alt * FEET_TO_METER, &sl_radius2, &tmp_lat_geoc );
+ sgGeodToGeoc( lat_geod, alt * SG_FEET_TO_METER, &sl_radius2, &tmp_lat_geoc );
- FG_LOG( FG_FLIGHT, FG_DEBUG, "lon = " << lon
+ SG_LOG( SG_FLIGHT, SG_DEBUG, "lon = " << lon
<< " lat_geod = " << lat_geod
<< " lat_geoc = " << lat_geoc
<< " alt = " << alt
- << " tmp_alt = " << tmp_alt * METER_TO_FEET
- << " sl_radius1 = " << sl_radius1 * METER_TO_FEET
- << " sl_radius2 = " << sl_radius2 * METER_TO_FEET
+ << " tmp_alt = " << tmp_alt * SG_METER_TO_FEET
+ << " sl_radius1 = " << sl_radius1 * SG_METER_TO_FEET
+ << " sl_radius2 = " << sl_radius2 * SG_METER_TO_FEET
<< " Equator = " << SG_EQUATORIAL_RADIUS_FT );
_set_Geocentric_Position( lat_geoc, lon,
- sl_radius2 * METER_TO_FEET + alt );
+ sl_radius2 * SG_METER_TO_FEET + alt );
_set_Geodetic_Position( lat_geod, lon, alt );
- _set_Sea_level_radius( sl_radius2 * METER_TO_FEET );
+ _set_Sea_level_radius( sl_radius2 * SG_METER_TO_FEET );
_set_Runway_altitude( scenery.cur_elev*METERS_TO_FEET );
_set_sin_lat_geocentric( lat_geoc );
// Set the altitude (force)
void fgFDMForceAltitude(const string &model, double alt_meters) {
+ SG_LOG(SG_FLIGHT,SG_INFO, "fgFDMForceAltitude: " << alt_meters );
+
double sea_level_radius_meters;
double lat_geoc;
sgGeodToGeoc( base_fdm_state.get_Latitude(), alt_meters,
&sea_level_radius_meters, &lat_geoc);
- base_fdm_state.set_Altitude( alt_meters * METER_TO_FEET );
+ base_fdm_state.set_Altitude( alt_meters * SG_METER_TO_FEET );
base_fdm_state.set_Sea_level_radius( sea_level_radius_meters *
- METER_TO_FEET );
-
+ SG_METER_TO_FEET );
+
+ cur_fdm_state->set_Altitude( alt_meters * SG_METER_TO_FEET );
+ cur_fdm_state->set_Sea_level_radius( sea_level_radius_meters *
+ SG_METER_TO_FEET );
// additional work needed for some flight models
if ( model == "larcsim" ) {
// Set the local ground elevation
void fgFDMSetGroundElevation(const string &model, double ground_meters) {
- FG_LOG( FG_FLIGHT,FG_INFO, "fgFDMSetGroundElevation: "
- << ground_meters*METER_TO_FEET );
- base_fdm_state.set_Runway_altitude( ground_meters * METER_TO_FEET );
- cur_fdm_state->set_Runway_altitude( ground_meters * METER_TO_FEET );
+ SG_LOG( SG_FLIGHT,SG_INFO, "fgFDMSetGroundElevation: "
+ << ground_meters*SG_METER_TO_FEET );
+ base_fdm_state.set_Runway_altitude( ground_meters * SG_METER_TO_FEET );
+ cur_fdm_state->set_Runway_altitude( ground_meters * SG_METER_TO_FEET );
}
void FGInterface::_busdump(void) {
- FG_LOG(FG_FLIGHT,FG_INFO,"d_pilot_rp_body_v[3]: " << d_pilot_rp_body_v[0] << ", " << d_pilot_rp_body_v[1] << ", " << d_pilot_rp_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"d_cg_rp_body_v[3]: " << d_cg_rp_body_v[0] << ", " << d_cg_rp_body_v[1] << ", " << d_cg_rp_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"f_body_total_v[3]: " << f_body_total_v[0] << ", " << f_body_total_v[1] << ", " << f_body_total_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"f_local_total_v[3]: " << f_local_total_v[0] << ", " << f_local_total_v[1] << ", " << f_local_total_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"f_aero_v[3]: " << f_aero_v[0] << ", " << f_aero_v[1] << ", " << f_aero_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"f_engine_v[3]: " << f_engine_v[0] << ", " << f_engine_v[1] << ", " << f_engine_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"f_gear_v[3]: " << f_gear_v[0] << ", " << f_gear_v[1] << ", " << f_gear_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"m_total_rp_v[3]: " << m_total_rp_v[0] << ", " << m_total_rp_v[1] << ", " << m_total_rp_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"m_total_cg_v[3]: " << m_total_cg_v[0] << ", " << m_total_cg_v[1] << ", " << m_total_cg_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"m_aero_v[3]: " << m_aero_v[0] << ", " << m_aero_v[1] << ", " << m_aero_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"m_engine_v[3]: " << m_engine_v[0] << ", " << m_engine_v[1] << ", " << m_engine_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"m_gear_v[3]: " << m_gear_v[0] << ", " << m_gear_v[1] << ", " << m_gear_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"v_dot_local_v[3]: " << v_dot_local_v[0] << ", " << v_dot_local_v[1] << ", " << v_dot_local_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"v_dot_body_v[3]: " << v_dot_body_v[0] << ", " << v_dot_body_v[1] << ", " << v_dot_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"a_cg_body_v[3]: " << a_cg_body_v[0] << ", " << a_cg_body_v[1] << ", " << a_cg_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"a_pilot_body_v[3]: " << a_pilot_body_v[0] << ", " << a_pilot_body_v[1] << ", " << a_pilot_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"n_cg_body_v[3]: " << n_cg_body_v[0] << ", " << n_cg_body_v[1] << ", " << n_cg_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"n_pilot_body_v[3]: " << n_pilot_body_v[0] << ", " << n_pilot_body_v[1] << ", " << n_pilot_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"omega_dot_body_v[3]: " << omega_dot_body_v[0] << ", " << omega_dot_body_v[1] << ", " << omega_dot_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"v_local_v[3]: " << v_local_v[0] << ", " << v_local_v[1] << ", " << v_local_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"v_local_rel_ground_v[3]: " << v_local_rel_ground_v[0] << ", " << v_local_rel_ground_v[1] << ", " << v_local_rel_ground_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"v_local_airmass_v[3]: " << v_local_airmass_v[0] << ", " << v_local_airmass_v[1] << ", " << v_local_airmass_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"v_local_rel_airmass_v[3]: " << v_local_rel_airmass_v[0] << ", " << v_local_rel_airmass_v[1] << ", " << v_local_rel_airmass_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"v_local_gust_v[3]: " << v_local_gust_v[0] << ", " << v_local_gust_v[1] << ", " << v_local_gust_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"v_wind_body_v[3]: " << v_wind_body_v[0] << ", " << v_wind_body_v[1] << ", " << v_wind_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"omega_body_v[3]: " << omega_body_v[0] << ", " << omega_body_v[1] << ", " << omega_body_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"omega_local_v[3]: " << omega_local_v[0] << ", " << omega_local_v[1] << ", " << omega_local_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"omega_total_v[3]: " << omega_total_v[0] << ", " << omega_total_v[1] << ", " << omega_total_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"euler_rates_v[3]: " << euler_rates_v[0] << ", " << euler_rates_v[1] << ", " << euler_rates_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"geocentric_rates_v[3]: " << geocentric_rates_v[0] << ", " << geocentric_rates_v[1] << ", " << geocentric_rates_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"geocentric_position_v[3]: " << geocentric_position_v[0] << ", " << geocentric_position_v[1] << ", " << geocentric_position_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"geodetic_position_v[3]: " << geodetic_position_v[0] << ", " << geodetic_position_v[1] << ", " << geodetic_position_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"euler_angles_v[3]: " << euler_angles_v[0] << ", " << euler_angles_v[1] << ", " << euler_angles_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"d_cg_rwy_local_v[3]: " << d_cg_rwy_local_v[0] << ", " << d_cg_rwy_local_v[1] << ", " << d_cg_rwy_local_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"d_cg_rwy_rwy_v[3]: " << d_cg_rwy_rwy_v[0] << ", " << d_cg_rwy_rwy_v[1] << ", " << d_cg_rwy_rwy_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"d_pilot_rwy_local_v[3]: " << d_pilot_rwy_local_v[0] << ", " << d_pilot_rwy_local_v[1] << ", " << d_pilot_rwy_local_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"d_pilot_rwy_rwy_v[3]: " << d_pilot_rwy_rwy_v[0] << ", " << d_pilot_rwy_rwy_v[1] << ", " << d_pilot_rwy_rwy_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"d_pilot_rp_body_v[3]: " << d_pilot_rp_body_v[0] << ", " << d_pilot_rp_body_v[1] << ", " << d_pilot_rp_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"d_cg_rp_body_v[3]: " << d_cg_rp_body_v[0] << ", " << d_cg_rp_body_v[1] << ", " << d_cg_rp_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"f_body_total_v[3]: " << f_body_total_v[0] << ", " << f_body_total_v[1] << ", " << f_body_total_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"f_local_total_v[3]: " << f_local_total_v[0] << ", " << f_local_total_v[1] << ", " << f_local_total_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"f_aero_v[3]: " << f_aero_v[0] << ", " << f_aero_v[1] << ", " << f_aero_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"f_engine_v[3]: " << f_engine_v[0] << ", " << f_engine_v[1] << ", " << f_engine_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"f_gear_v[3]: " << f_gear_v[0] << ", " << f_gear_v[1] << ", " << f_gear_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"m_total_rp_v[3]: " << m_total_rp_v[0] << ", " << m_total_rp_v[1] << ", " << m_total_rp_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"m_total_cg_v[3]: " << m_total_cg_v[0] << ", " << m_total_cg_v[1] << ", " << m_total_cg_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"m_aero_v[3]: " << m_aero_v[0] << ", " << m_aero_v[1] << ", " << m_aero_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"m_engine_v[3]: " << m_engine_v[0] << ", " << m_engine_v[1] << ", " << m_engine_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"m_gear_v[3]: " << m_gear_v[0] << ", " << m_gear_v[1] << ", " << m_gear_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_dot_local_v[3]: " << v_dot_local_v[0] << ", " << v_dot_local_v[1] << ", " << v_dot_local_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_dot_body_v[3]: " << v_dot_body_v[0] << ", " << v_dot_body_v[1] << ", " << v_dot_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"a_cg_body_v[3]: " << a_cg_body_v[0] << ", " << a_cg_body_v[1] << ", " << a_cg_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"a_pilot_body_v[3]: " << a_pilot_body_v[0] << ", " << a_pilot_body_v[1] << ", " << a_pilot_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"n_cg_body_v[3]: " << n_cg_body_v[0] << ", " << n_cg_body_v[1] << ", " << n_cg_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"n_pilot_body_v[3]: " << n_pilot_body_v[0] << ", " << n_pilot_body_v[1] << ", " << n_pilot_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"omega_dot_body_v[3]: " << omega_dot_body_v[0] << ", " << omega_dot_body_v[1] << ", " << omega_dot_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_local_v[3]: " << v_local_v[0] << ", " << v_local_v[1] << ", " << v_local_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_local_rel_ground_v[3]: " << v_local_rel_ground_v[0] << ", " << v_local_rel_ground_v[1] << ", " << v_local_rel_ground_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_local_airmass_v[3]: " << v_local_airmass_v[0] << ", " << v_local_airmass_v[1] << ", " << v_local_airmass_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_local_rel_airmass_v[3]: " << v_local_rel_airmass_v[0] << ", " << v_local_rel_airmass_v[1] << ", " << v_local_rel_airmass_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_local_gust_v[3]: " << v_local_gust_v[0] << ", " << v_local_gust_v[1] << ", " << v_local_gust_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_wind_body_v[3]: " << v_wind_body_v[0] << ", " << v_wind_body_v[1] << ", " << v_wind_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"omega_body_v[3]: " << omega_body_v[0] << ", " << omega_body_v[1] << ", " << omega_body_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"omega_local_v[3]: " << omega_local_v[0] << ", " << omega_local_v[1] << ", " << omega_local_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"omega_total_v[3]: " << omega_total_v[0] << ", " << omega_total_v[1] << ", " << omega_total_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"euler_rates_v[3]: " << euler_rates_v[0] << ", " << euler_rates_v[1] << ", " << euler_rates_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"geocentric_rates_v[3]: " << geocentric_rates_v[0] << ", " << geocentric_rates_v[1] << ", " << geocentric_rates_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"geocentric_position_v[3]: " << geocentric_position_v[0] << ", " << geocentric_position_v[1] << ", " << geocentric_position_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"geodetic_position_v[3]: " << geodetic_position_v[0] << ", " << geodetic_position_v[1] << ", " << geodetic_position_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"euler_angles_v[3]: " << euler_angles_v[0] << ", " << euler_angles_v[1] << ", " << euler_angles_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"d_cg_rwy_local_v[3]: " << d_cg_rwy_local_v[0] << ", " << d_cg_rwy_local_v[1] << ", " << d_cg_rwy_local_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"d_cg_rwy_rwy_v[3]: " << d_cg_rwy_rwy_v[0] << ", " << d_cg_rwy_rwy_v[1] << ", " << d_cg_rwy_rwy_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"d_pilot_rwy_local_v[3]: " << d_pilot_rwy_local_v[0] << ", " << d_pilot_rwy_local_v[1] << ", " << d_pilot_rwy_local_v[2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"d_pilot_rwy_rwy_v[3]: " << d_pilot_rwy_rwy_v[0] << ", " << d_pilot_rwy_rwy_v[1] << ", " << d_pilot_rwy_rwy_v[2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"t_local_to_body_m[0][3]: " << t_local_to_body_m[0][0] << ", " << t_local_to_body_m[0][1] << ", " << t_local_to_body_m[0][2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"t_local_to_body_m[1][3]: " << t_local_to_body_m[1][0] << ", " << t_local_to_body_m[1][1] << ", " << t_local_to_body_m[1][2]);
- FG_LOG(FG_FLIGHT,FG_INFO,"t_local_to_body_m[2][3]: " << t_local_to_body_m[2][0] << ", " << t_local_to_body_m[2][1] << ", " << t_local_to_body_m[2][2]);
-
- FG_LOG(FG_FLIGHT,FG_INFO,"mass: " << mass );
- FG_LOG(FG_FLIGHT,FG_INFO,"i_xx: " << i_xx );
- FG_LOG(FG_FLIGHT,FG_INFO,"i_yy: " << i_yy );
- FG_LOG(FG_FLIGHT,FG_INFO,"i_zz: " << i_zz );
- FG_LOG(FG_FLIGHT,FG_INFO,"i_xz: " << i_xz );
- FG_LOG(FG_FLIGHT,FG_INFO,"nlf: " << nlf );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_rel_wind: " << v_rel_wind );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_true_kts: " << v_true_kts );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_rel_ground: " << v_rel_ground );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_inertial: " << v_inertial );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_ground_speed: " << v_ground_speed );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_equiv: " << v_equiv );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_equiv_kts: " << v_equiv_kts );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_calibrated: " << v_calibrated );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_calibrated_kts: " << v_calibrated_kts );
- FG_LOG(FG_FLIGHT,FG_INFO,"gravity: " << gravity );
- FG_LOG(FG_FLIGHT,FG_INFO,"centrifugal_relief: " << centrifugal_relief );
- FG_LOG(FG_FLIGHT,FG_INFO,"alpha: " << alpha );
- FG_LOG(FG_FLIGHT,FG_INFO,"beta: " << beta );
- FG_LOG(FG_FLIGHT,FG_INFO,"alpha_dot: " << alpha_dot );
- FG_LOG(FG_FLIGHT,FG_INFO,"beta_dot: " << beta_dot );
- FG_LOG(FG_FLIGHT,FG_INFO,"cos_alpha: " << cos_alpha );
- FG_LOG(FG_FLIGHT,FG_INFO,"sin_alpha: " << sin_alpha );
- FG_LOG(FG_FLIGHT,FG_INFO,"cos_beta: " << cos_beta );
- FG_LOG(FG_FLIGHT,FG_INFO,"sin_beta: " << sin_beta );
- FG_LOG(FG_FLIGHT,FG_INFO,"cos_phi: " << cos_phi );
- FG_LOG(FG_FLIGHT,FG_INFO,"sin_phi: " << sin_phi );
- FG_LOG(FG_FLIGHT,FG_INFO,"cos_theta: " << cos_theta );
- FG_LOG(FG_FLIGHT,FG_INFO,"sin_theta: " << sin_theta );
- FG_LOG(FG_FLIGHT,FG_INFO,"cos_psi: " << cos_psi );
- FG_LOG(FG_FLIGHT,FG_INFO,"sin_psi: " << sin_psi );
- FG_LOG(FG_FLIGHT,FG_INFO,"gamma_vert_rad: " << gamma_vert_rad );
- FG_LOG(FG_FLIGHT,FG_INFO,"gamma_horiz_rad: " << gamma_horiz_rad );
- FG_LOG(FG_FLIGHT,FG_INFO,"sigma: " << sigma );
- FG_LOG(FG_FLIGHT,FG_INFO,"density: " << density );
- FG_LOG(FG_FLIGHT,FG_INFO,"v_sound: " << v_sound );
- FG_LOG(FG_FLIGHT,FG_INFO,"mach_number: " << mach_number );
- FG_LOG(FG_FLIGHT,FG_INFO,"static_pressure: " << static_pressure );
- FG_LOG(FG_FLIGHT,FG_INFO,"total_pressure: " << total_pressure );
- FG_LOG(FG_FLIGHT,FG_INFO,"impact_pressure: " << impact_pressure );
- FG_LOG(FG_FLIGHT,FG_INFO,"dynamic_pressure: " << dynamic_pressure );
- FG_LOG(FG_FLIGHT,FG_INFO,"static_temperature: " << static_temperature );
- FG_LOG(FG_FLIGHT,FG_INFO,"total_temperature: " << total_temperature );
- FG_LOG(FG_FLIGHT,FG_INFO,"sea_level_radius: " << sea_level_radius );
- FG_LOG(FG_FLIGHT,FG_INFO,"earth_position_angle: " << earth_position_angle );
- FG_LOG(FG_FLIGHT,FG_INFO,"runway_altitude: " << runway_altitude );
- FG_LOG(FG_FLIGHT,FG_INFO,"runway_latitude: " << runway_latitude );
- FG_LOG(FG_FLIGHT,FG_INFO,"runway_longitude: " << runway_longitude );
- FG_LOG(FG_FLIGHT,FG_INFO,"runway_heading: " << runway_heading );
- FG_LOG(FG_FLIGHT,FG_INFO,"radius_to_rwy: " << radius_to_rwy );
- FG_LOG(FG_FLIGHT,FG_INFO,"climb_rate: " << climb_rate );
- FG_LOG(FG_FLIGHT,FG_INFO,"sin_lat_geocentric: " << sin_lat_geocentric );
- FG_LOG(FG_FLIGHT,FG_INFO,"cos_lat_geocentric: " << cos_lat_geocentric );
- FG_LOG(FG_FLIGHT,FG_INFO,"sin_longitude: " << sin_longitude );
- FG_LOG(FG_FLIGHT,FG_INFO,"cos_longitude: " << cos_longitude );
- FG_LOG(FG_FLIGHT,FG_INFO,"sin_latitude: " << sin_latitude );
- FG_LOG(FG_FLIGHT,FG_INFO,"cos_latitude: " << cos_latitude );
- FG_LOG(FG_FLIGHT,FG_INFO,"altitude_agl: " << altitude_agl );
+ SG_LOG(SG_FLIGHT,SG_INFO,"t_local_to_body_m[0][3]: " << t_local_to_body_m[0][0] << ", " << t_local_to_body_m[0][1] << ", " << t_local_to_body_m[0][2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"t_local_to_body_m[1][3]: " << t_local_to_body_m[1][0] << ", " << t_local_to_body_m[1][1] << ", " << t_local_to_body_m[1][2]);
+ SG_LOG(SG_FLIGHT,SG_INFO,"t_local_to_body_m[2][3]: " << t_local_to_body_m[2][0] << ", " << t_local_to_body_m[2][1] << ", " << t_local_to_body_m[2][2]);
+
+ SG_LOG(SG_FLIGHT,SG_INFO,"mass: " << mass );
+ SG_LOG(SG_FLIGHT,SG_INFO,"i_xx: " << i_xx );
+ SG_LOG(SG_FLIGHT,SG_INFO,"i_yy: " << i_yy );
+ SG_LOG(SG_FLIGHT,SG_INFO,"i_zz: " << i_zz );
+ SG_LOG(SG_FLIGHT,SG_INFO,"i_xz: " << i_xz );
+ SG_LOG(SG_FLIGHT,SG_INFO,"nlf: " << nlf );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_rel_wind: " << v_rel_wind );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_true_kts: " << v_true_kts );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_rel_ground: " << v_rel_ground );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_inertial: " << v_inertial );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_ground_speed: " << v_ground_speed );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_equiv: " << v_equiv );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_equiv_kts: " << v_equiv_kts );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_calibrated: " << v_calibrated );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_calibrated_kts: " << v_calibrated_kts );
+ SG_LOG(SG_FLIGHT,SG_INFO,"gravity: " << gravity );
+ SG_LOG(SG_FLIGHT,SG_INFO,"centrifugal_relief: " << centrifugal_relief );
+ SG_LOG(SG_FLIGHT,SG_INFO,"alpha: " << alpha );
+ SG_LOG(SG_FLIGHT,SG_INFO,"beta: " << beta );
+ SG_LOG(SG_FLIGHT,SG_INFO,"alpha_dot: " << alpha_dot );
+ SG_LOG(SG_FLIGHT,SG_INFO,"beta_dot: " << beta_dot );
+ SG_LOG(SG_FLIGHT,SG_INFO,"cos_alpha: " << cos_alpha );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sin_alpha: " << sin_alpha );
+ SG_LOG(SG_FLIGHT,SG_INFO,"cos_beta: " << cos_beta );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sin_beta: " << sin_beta );
+ SG_LOG(SG_FLIGHT,SG_INFO,"cos_phi: " << cos_phi );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sin_phi: " << sin_phi );
+ SG_LOG(SG_FLIGHT,SG_INFO,"cos_theta: " << cos_theta );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sin_theta: " << sin_theta );
+ SG_LOG(SG_FLIGHT,SG_INFO,"cos_psi: " << cos_psi );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sin_psi: " << sin_psi );
+ SG_LOG(SG_FLIGHT,SG_INFO,"gamma_vert_rad: " << gamma_vert_rad );
+ SG_LOG(SG_FLIGHT,SG_INFO,"gamma_horiz_rad: " << gamma_horiz_rad );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sigma: " << sigma );
+ SG_LOG(SG_FLIGHT,SG_INFO,"density: " << density );
+ SG_LOG(SG_FLIGHT,SG_INFO,"v_sound: " << v_sound );
+ SG_LOG(SG_FLIGHT,SG_INFO,"mach_number: " << mach_number );
+ SG_LOG(SG_FLIGHT,SG_INFO,"static_pressure: " << static_pressure );
+ SG_LOG(SG_FLIGHT,SG_INFO,"total_pressure: " << total_pressure );
+ SG_LOG(SG_FLIGHT,SG_INFO,"impact_pressure: " << impact_pressure );
+ SG_LOG(SG_FLIGHT,SG_INFO,"dynamic_pressure: " << dynamic_pressure );
+ SG_LOG(SG_FLIGHT,SG_INFO,"static_temperature: " << static_temperature );
+ SG_LOG(SG_FLIGHT,SG_INFO,"total_temperature: " << total_temperature );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sea_level_radius: " << sea_level_radius );
+ SG_LOG(SG_FLIGHT,SG_INFO,"earth_position_angle: " << earth_position_angle );
+ SG_LOG(SG_FLIGHT,SG_INFO,"runway_altitude: " << runway_altitude );
+ SG_LOG(SG_FLIGHT,SG_INFO,"runway_latitude: " << runway_latitude );
+ SG_LOG(SG_FLIGHT,SG_INFO,"runway_longitude: " << runway_longitude );
+ SG_LOG(SG_FLIGHT,SG_INFO,"runway_heading: " << runway_heading );
+ SG_LOG(SG_FLIGHT,SG_INFO,"radius_to_rwy: " << radius_to_rwy );
+ SG_LOG(SG_FLIGHT,SG_INFO,"climb_rate: " << climb_rate );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sin_lat_geocentric: " << sin_lat_geocentric );
+ SG_LOG(SG_FLIGHT,SG_INFO,"cos_lat_geocentric: " << cos_lat_geocentric );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sin_longitude: " << sin_longitude );
+ SG_LOG(SG_FLIGHT,SG_INFO,"cos_longitude: " << cos_longitude );
+ SG_LOG(SG_FLIGHT,SG_INFO,"sin_latitude: " << sin_latitude );
+ SG_LOG(SG_FLIGHT,SG_INFO,"cos_latitude: " << cos_latitude );
+ SG_LOG(SG_FLIGHT,SG_INFO,"altitude_agl: " << altitude_agl );
}
+
+void fgToggleFDMdataLogging(void) {
+ cur_fdm_state->ToggleDataLogging();
+}
+