1 // flight.c -- a general interface to the various flight models
3 // Written by Curtis Olson, started May 1997.
5 // Copyright (C) 1997 Curtis L. Olson - curt@infoplane.com
7 // This program is free software; you can redistribute it and/or
8 // modify it under the terms of the GNU 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.
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 // General Public License for more details.
17 // You should have received a copy of the GNU General Public License
18 // along with this program; if not, write to the Free Software
19 // Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
26 #include <simgear/constants.h>
27 #include <simgear/debug/logstream.hxx>
28 #include <simgear/math/sg_geodesy.hxx>
29 #include <simgear/timing/timestamp.hxx>
31 #include <Scenery/scenery.hxx>
32 #include <FDM/LaRCsim/ls_interface.h>
33 #include <Main/globals.hxx>
34 #include <Main/fg_props.hxx>
36 #include "External.hxx"
39 #include "LaRCsim.hxx"
43 // base_fdm_state is the internal state that is updated in integer
44 // multiples of "dt". This leads to "jitter" with respect to the real
45 // world time, so we introduce cur_fdm_state which is extrapolated by
46 // the difference between sim time and real world time
48 FGInterface *cur_fdm_state;
49 FGInterface base_fdm_state;
51 inline void init_vec(FG_VECTOR_3 vec) {
52 vec[0] = 0.0; vec[1] = 0.0; vec[2] = 0.0;
55 FGEngInterface::FGEngInterface() {
71 FGEngInterface::~FGEngInterface(void) {
76 FGInterface::FGInterface() {
80 FGInterface::FGInterface( double dt ) {
84 remainder = elapsed = multi_loop = 0;
88 FGInterface::~FGInterface() {
89 // unbind(); // FIXME: should be called explicitly
94 * Set default values for the state of the FDM.
96 * This method is invoked by the constructors.
99 FGInterface::_setup ()
101 init_vec( d_pilot_rp_body_v );
102 init_vec( d_cg_rp_body_v );
103 init_vec( f_body_total_v );
104 init_vec( f_local_total_v );
105 init_vec( f_aero_v );
106 init_vec( f_engine_v );
107 init_vec( f_gear_v );
108 init_vec( m_total_rp_v );
109 init_vec( m_total_cg_v );
110 init_vec( m_aero_v );
111 init_vec( m_engine_v );
112 init_vec( m_gear_v );
113 init_vec( v_dot_local_v );
114 init_vec( v_dot_body_v );
115 init_vec( a_cg_body_v );
116 init_vec( a_pilot_body_v );
117 init_vec( n_cg_body_v );
118 init_vec( n_pilot_body_v );
119 init_vec( omega_dot_body_v );
120 init_vec( v_local_v );
121 init_vec( v_local_rel_ground_v );
122 init_vec( v_local_airmass_v );
123 init_vec( v_local_rel_airmass_v );
124 init_vec( v_local_gust_v );
125 init_vec( v_wind_body_v );
126 init_vec( omega_body_v );
127 init_vec( omega_local_v );
128 init_vec( omega_total_v );
129 init_vec( euler_rates_v );
130 init_vec( geocentric_rates_v );
131 init_vec( geocentric_position_v );
132 init_vec( geodetic_position_v );
133 init_vec( euler_angles_v );
134 init_vec( d_cg_rwy_local_v );
135 init_vec( d_cg_rwy_rwy_v );
136 init_vec( d_pilot_rwy_local_v );
137 init_vec( d_pilot_rwy_rwy_v );
138 init_vec( t_local_to_body_m[0] );
139 init_vec( t_local_to_body_m[1] );
140 init_vec( t_local_to_body_m[2] );
142 mass=i_xx=i_yy=i_zz=i_xz=0;
144 v_rel_wind=v_true_kts=v_rel_ground=v_inertial=0;
145 v_ground_speed=v_equiv=v_equiv_kts=0;
146 v_calibrated=v_calibrated_kts=0;
148 centrifugal_relief=0;
149 alpha=beta=alpha_dot=beta_dot=0;
150 cos_alpha=sin_alpha=cos_beta=sin_beta=0;
151 cos_phi=sin_phi=cos_theta=sin_theta=cos_psi=sin_psi=0;
152 gamma_vert_rad=gamma_horiz_rad=0;
153 sigma=density=v_sound=mach_number=0;
154 static_pressure=total_pressure=impact_pressure=0;
156 static_temperature=total_temperature=0;
157 sea_level_radius=earth_position_angle=0;
158 runway_altitude=runway_latitude=runway_longitude=0;
162 sin_lat_geocentric=cos_lat_geocentric=0;
163 sin_latitude=cos_latitude=0;
164 sin_longitude=cos_longitude=0;
170 * Initialize the state of the FDM.
172 * Subclasses of FGInterface may do their own, additional initialization,
173 * but normally they should invoke this method explicitly first as
174 * FGInterface::init() to make sure the basic structures are set up
180 SG_LOG(SG_FLIGHT, SG_INFO, "Start initializing FGInterface");
185 // Set initial position
186 SG_LOG(SG_FLIGHT, SG_INFO, "...initializing position...");
187 set_Longitude(fgGetDouble("/position/longitude") * SGD_DEGREES_TO_RADIANS);
188 set_Latitude(fgGetDouble("/position/latitude") * SGD_DEGREES_TO_RADIANS);
189 double ground_elev_m = scenery.cur_elev + 1;
190 double ground_elev_ft = ground_elev_m * METERS_TO_FEET;
191 if (fgGetBool("/sim/startup/onground") ||
192 fgGetDouble("/position/altitude") < ground_elev_ft)
193 fgSetDouble("/position/altitude", ground_elev_ft);
194 set_Altitude(fgGetDouble("/position/altitude"));
196 // Set ground elevation
197 SG_LOG(SG_FLIGHT, SG_INFO,
198 "...initializing ground elevation to "
199 << ground_elev_ft << "ft...");
200 fgFDMSetGroundElevation("jsb", ground_elev_m);
202 // Set sea-level radius
203 SG_LOG(SG_FLIGHT, SG_INFO, "...initializing sea-level radius...");
204 double sea_level_radius_meters;
206 sgGeodToGeoc(get_Latitude(), get_Altitude(),
207 &sea_level_radius_meters, &lat_geoc);
208 set_Sea_level_radius(sea_level_radius_meters * SG_METER_TO_FEET);
210 // Set initial velocities
211 SG_LOG(SG_FLIGHT, SG_INFO, "...initializing velocities...");
212 if (!fgHasValue("/sim/startup/speed-set")) {
213 set_V_calibrated_kts(0.0);
215 const string speedset = fgGetString("/sim/startup/speed-set");
216 if (speedset == "knots" || speedset == "KNOTS") {
217 set_V_calibrated_kts(fgGetDouble("/velocities/airspeed"));
218 } else if (speedset == "mach" || speedset == "MACH") {
219 set_Mach_number(fgGetDouble("/velocities/mach"));
220 } else if (speedset == "UVW" || speedset == "uvw") {
221 set_Velocities_Wind_Body(fgGetDouble("/velocities/uBody"),
222 fgGetDouble("/velocities/vBody"),
223 fgGetDouble("/velocities/wBody"));
224 } else if (speedset == "NED" || speedset == "ned") {
225 set_Velocities_Local(fgGetDouble("/velocities/speed-north"),
226 fgGetDouble("/velocities/speed-east"),
227 fgGetDouble("/velocities/speed-down"));
229 SG_LOG(SG_FLIGHT, SG_ALERT,
230 "Unrecognized value for /sim/startup/speed-set: " << speedset);
231 set_V_calibrated_kts(0.0);
235 // Set initial Euler angles
236 SG_LOG(SG_FLIGHT, SG_INFO, "...initializing Euler angles...");
238 (fgGetDouble("/orientation/roll") * SGD_DEGREES_TO_RADIANS,
239 fgGetDouble("/orientation/pitch") * SGD_DEGREES_TO_RADIANS,
240 fgGetDouble("/orientation/heading") * SGD_DEGREES_TO_RADIANS);
242 SG_LOG(SG_FLIGHT, SG_INFO, "End initializing FGInterface");
247 * Bind getters and setters to properties.
249 * The bind() method will be invoked after init(). Note that unlike
250 * the usual implementations of FGSubsystem::bind(), this method does
251 * not automatically pick up existing values for the properties at
252 * bind time; instead, all values are set explicitly in the init()
258 // Time management (read-only)
259 fgTie("/fdm/time/delta_t", this,
260 &FGInterface::get_delta_t); // read-only
261 fgTie("/fdm/time/elapsed", this,
262 &FGInterface::get_elapsed); // read-only
263 fgTie("/fdm/time/remainder", this,
264 &FGInterface::get_remainder); // read-only
265 fgTie("/fdm/time/multi_loop", this,
266 &FGInterface::get_multi_loop); // read-only
269 fgTie("/position/latitude", this,
270 &FGInterface::get_Latitude_deg,
271 &FGInterface::set_Latitude_deg,
273 fgTie("/position/longitude", this,
274 &FGInterface::get_Longitude_deg,
275 &FGInterface::set_Longitude_deg,
277 fgTie("/position/altitude", this,
278 &FGInterface::get_Altitude,
279 &FGInterface::set_Altitude,
281 fgTie("/position/altitude-agl", this,
282 &FGInterface::get_Altitude_AGL); // read-only
285 fgTie("/orientation/roll", this,
286 &FGInterface::get_Phi_deg,
287 &FGInterface::set_Phi_deg);
288 fgTie("/orientation/pitch", this,
289 &FGInterface::get_Theta_deg,
290 &FGInterface::set_Theta_deg);
291 fgTie("/orientation/heading", this,
292 &FGInterface::get_Psi_deg,
293 &FGInterface::set_Psi_deg);
295 // Calibrated airspeed
296 fgTie("/velocities/airspeed", this,
297 &FGInterface::get_V_calibrated_kts,
298 &FGInterface::set_V_calibrated_kts);
301 fgTie("/velocities/speed-north", this,
302 &FGInterface::get_V_north,
303 &FGInterface::set_V_north);
304 fgTie("/velocities/speed-east", this,
305 &FGInterface::get_V_east,
306 &FGInterface::set_V_east);
307 fgTie("/velocities/speed-down", this,
308 &FGInterface::get_V_down,
309 &FGInterface::set_V_down);
312 fgTie("/velocities/uBody", this,
313 &FGInterface::get_uBody,
314 &FGInterface::set_uBody);
315 fgTie("/velocities/vBody", this,
316 &FGInterface::get_vBody,
317 &FGInterface::set_vBody);
318 fgTie("/velocities/wBody", this,
319 &FGInterface::get_wBody,
320 &FGInterface::set_wBody);
322 // Climb and slip (read-only)
323 fgTie("/velocities/vertical-speed", this,
324 &FGInterface::get_Climb_Rate); // read-only
325 fgTie("/velocities/side-slip", this,
326 &FGInterface::get_Beta); // read-only
331 * Unbind any properties bound to this FDM.
333 * This method allows the FDM to release properties so that a new
334 * FDM can bind them instead.
337 FGInterface::unbind ()
339 fgUntie("/fdm/time/delta_t");
340 fgUntie("/fdm/time/elapsed");
341 fgUntie("/fdm/time/remainder");
342 fgUntie("/fdm/time/multi_loop");
343 fgUntie("/position/latitude");
344 fgUntie("/position/longitude");
345 fgUntie("/position/altitude");
346 fgUntie("/position/heading");
347 fgUntie("/position/pitch");
348 fgUntie("/position/roll");
349 fgUntie("/velocities/airspeed");
350 fgUntie("/velocities/speed-north");
351 fgUntie("/velocities/speed-east");
352 fgUntie("/velocities/speed-down");
353 fgUntie("/velocities/uBody");
354 fgUntie("/velocities/vBody");
355 fgUntie("/velocities/wBody");
356 fgUntie("/velocities/vertical-speed");
357 fgUntie("/velocities/side-slip");
362 * Update the state of the FDM (i.e. run the equations of motion).
365 FGInterface::update ()
371 bool FGInterface::update( int multi_loop ) {
372 cout << "dummy update() ... SHOULDN'T BE CALLED!" << endl;
377 void FGInterface::_updatePosition( double lat_geoc, double lon, double alt ) {
378 double lat_geod, tmp_alt, sl_radius1, sl_radius2, tmp_lat_geoc;
380 sgGeocToGeod( lat_geoc, ( get_Sea_level_radius() + alt ) * SG_FEET_TO_METER,
381 &lat_geod, &tmp_alt, &sl_radius1 );
382 sgGeodToGeoc( lat_geod, alt * SG_FEET_TO_METER, &sl_radius2, &tmp_lat_geoc );
384 SG_LOG( SG_FLIGHT, SG_DEBUG, "lon = " << lon
385 << " lat_geod = " << lat_geod
386 << " lat_geoc = " << lat_geoc
388 << " tmp_alt = " << tmp_alt * SG_METER_TO_FEET
389 << " sl_radius1 = " << sl_radius1 * SG_METER_TO_FEET
390 << " sl_radius2 = " << sl_radius2 * SG_METER_TO_FEET
391 << " Equator = " << SG_EQUATORIAL_RADIUS_FT );
393 _set_Geocentric_Position( lat_geoc, lon,
394 sl_radius2 * SG_METER_TO_FEET + alt );
396 _set_Geodetic_Position( lat_geod, lon, alt );
398 _set_Sea_level_radius( sl_radius2 * SG_METER_TO_FEET );
399 _set_Runway_altitude( scenery.cur_elev*METERS_TO_FEET );
401 _set_sin_lat_geocentric( lat_geoc );
402 _set_cos_lat_geocentric( lat_geoc );
404 _set_sin_cos_longitude( lon );
406 _set_sin_cos_latitude( lat_geod );
408 /* Norman's code for slope of the terrain */
409 /* needs to be tested -- get it on the HUD and taxi around */
410 /* double *tnorm = scenery.cur_normal;
412 double sy = sin ( -get_Psi() ) ;
413 double cy = cos ( -get_Psi() ) ;
415 double phitb, thetatb, psitb;
416 if(tnorm[1] != 0.0) {
417 psitb = -atan2 ( tnorm[0], tnorm[1] );
419 if(tnorm[2] != 0.0) {
420 thetatb = atan2 ( tnorm[0] * cy - tnorm[1] * sy, tnorm[2] );
421 phitb = -atan2 ( tnorm[1] * cy + tnorm[0] * sy, tnorm[2] );
424 _set_terrain_slope(phitb, thetatb, psitb)
429 // Extrapolate fdm based on time_offset (in usec)
430 void FGInterface::extrapolate( int time_offset ) {
431 double dt = time_offset / 1000000.0;
433 // -dw- metrowerks complains about ambiguous access, not critical
436 cout << "extrapolating FDM by dt = " << dt << endl;
439 double lat = geodetic_position_v[0] + geocentric_rates_v[0] * dt;
440 double lat_geoc = geocentric_position_v[0] + geocentric_rates_v[0] * dt;
442 double lon = geodetic_position_v[1] + geocentric_rates_v[1] * dt;
443 double lon_geoc = geocentric_position_v[1] + geocentric_rates_v[1] * dt;
445 double alt = geodetic_position_v[2] + geocentric_rates_v[2] * dt;
446 double radius = geocentric_position_v[2] + geocentric_rates_v[2] * dt;
448 geodetic_position_v[0] = lat;
449 geocentric_position_v[0] = lat_geoc;
451 geodetic_position_v[1] = lon;
452 geocentric_position_v[1] = lon_geoc;
454 geodetic_position_v[2] = alt;
455 geocentric_position_v[2] = radius;
459 // Set the altitude (force)
460 void fgFDMForceAltitude(const string &model, double alt_meters) {
461 double sea_level_radius_meters;
464 // Set the FG variables first
465 sgGeodToGeoc( base_fdm_state.get_Latitude(), alt_meters,
466 &sea_level_radius_meters, &lat_geoc);
468 base_fdm_state.set_Altitude( alt_meters * SG_METER_TO_FEET );
469 base_fdm_state.set_Sea_level_radius( sea_level_radius_meters *
473 // additional work needed for some flight models
474 if ( model == "larcsim" ) {
475 ls_ForceAltitude( base_fdm_state.get_Altitude() );
480 // Set the local ground elevation
481 void fgFDMSetGroundElevation(const string &model, double ground_meters) {
482 SG_LOG( SG_FLIGHT,SG_INFO, "fgFDMSetGroundElevation: "
483 << ground_meters*SG_METER_TO_FEET );
484 base_fdm_state.set_Runway_altitude( ground_meters * SG_METER_TO_FEET );
485 cur_fdm_state->set_Runway_altitude( ground_meters * SG_METER_TO_FEET );
490 void FGInterface::set_Latitude(double lat) {
491 geodetic_position_v[0] = lat;
494 void FGInterface::set_Longitude(double lon) {
495 geodetic_position_v[1] = lon;
498 void FGInterface::set_Altitude(double alt) {
499 geodetic_position_v[2] = alt;
502 void FGInterface::set_AltitudeAGL(double altagl) {
507 void FGInterface::set_V_calibrated_kts(double vc) {
508 v_calibrated_kts = vc;
511 void FGInterface::set_Mach_number(double mach) {
515 void FGInterface::set_Velocities_Local( double north,
518 v_local_v[0] = north;
523 void FGInterface::set_Velocities_Wind_Body( double u,
526 v_wind_body_v[0] = u;
527 v_wind_body_v[1] = v;
528 v_wind_body_v[2] = w;
532 void FGInterface::set_Euler_Angles( double phi,
535 euler_angles_v[0] = phi;
536 euler_angles_v[1] = theta;
537 euler_angles_v[2] = psi;
541 void FGInterface::set_Climb_Rate( double roc) {
545 void FGInterface::set_Gamma_vert_rad( double gamma) {
546 gamma_vert_rad = gamma;
550 void FGInterface::set_Sea_level_radius(double slr) {
551 sea_level_radius = slr;
554 void FGInterface::set_Runway_altitude(double ralt) {
555 runway_altitude = ralt;
558 void FGInterface::set_Static_pressure(double p) { static_pressure = p; }
559 void FGInterface::set_Static_temperature(double T) { static_temperature = T; }
560 void FGInterface::set_Density(double rho) { density = rho; }
562 void FGInterface::set_Velocities_Local_Airmass (double wnorth,
565 v_local_airmass_v[0] = wnorth;
566 v_local_airmass_v[1] = weast;
567 v_local_airmass_v[2] = wdown;
571 void FGInterface::_busdump(void) {
573 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]);
574 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]);
575 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]);
576 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]);
577 SG_LOG(SG_FLIGHT,SG_INFO,"f_aero_v[3]: " << f_aero_v[0] << ", " << f_aero_v[1] << ", " << f_aero_v[2]);
578 SG_LOG(SG_FLIGHT,SG_INFO,"f_engine_v[3]: " << f_engine_v[0] << ", " << f_engine_v[1] << ", " << f_engine_v[2]);
579 SG_LOG(SG_FLIGHT,SG_INFO,"f_gear_v[3]: " << f_gear_v[0] << ", " << f_gear_v[1] << ", " << f_gear_v[2]);
580 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]);
581 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]);
582 SG_LOG(SG_FLIGHT,SG_INFO,"m_aero_v[3]: " << m_aero_v[0] << ", " << m_aero_v[1] << ", " << m_aero_v[2]);
583 SG_LOG(SG_FLIGHT,SG_INFO,"m_engine_v[3]: " << m_engine_v[0] << ", " << m_engine_v[1] << ", " << m_engine_v[2]);
584 SG_LOG(SG_FLIGHT,SG_INFO,"m_gear_v[3]: " << m_gear_v[0] << ", " << m_gear_v[1] << ", " << m_gear_v[2]);
585 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]);
586 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]);
587 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]);
588 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]);
589 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]);
590 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]);
591 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]);
592 SG_LOG(SG_FLIGHT,SG_INFO,"v_local_v[3]: " << v_local_v[0] << ", " << v_local_v[1] << ", " << v_local_v[2]);
593 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]);
594 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]);
595 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]);
596 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]);
597 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]);
598 SG_LOG(SG_FLIGHT,SG_INFO,"omega_body_v[3]: " << omega_body_v[0] << ", " << omega_body_v[1] << ", " << omega_body_v[2]);
599 SG_LOG(SG_FLIGHT,SG_INFO,"omega_local_v[3]: " << omega_local_v[0] << ", " << omega_local_v[1] << ", " << omega_local_v[2]);
600 SG_LOG(SG_FLIGHT,SG_INFO,"omega_total_v[3]: " << omega_total_v[0] << ", " << omega_total_v[1] << ", " << omega_total_v[2]);
601 SG_LOG(SG_FLIGHT,SG_INFO,"euler_rates_v[3]: " << euler_rates_v[0] << ", " << euler_rates_v[1] << ", " << euler_rates_v[2]);
602 SG_LOG(SG_FLIGHT,SG_INFO,"geocentric_rates_v[3]: " << geocentric_rates_v[0] << ", " << geocentric_rates_v[1] << ", " << geocentric_rates_v[2]);
603 SG_LOG(SG_FLIGHT,SG_INFO,"geocentric_position_v[3]: " << geocentric_position_v[0] << ", " << geocentric_position_v[1] << ", " << geocentric_position_v[2]);
604 SG_LOG(SG_FLIGHT,SG_INFO,"geodetic_position_v[3]: " << geodetic_position_v[0] << ", " << geodetic_position_v[1] << ", " << geodetic_position_v[2]);
605 SG_LOG(SG_FLIGHT,SG_INFO,"euler_angles_v[3]: " << euler_angles_v[0] << ", " << euler_angles_v[1] << ", " << euler_angles_v[2]);
606 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]);
607 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]);
608 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]);
609 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]);
611 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]);
612 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]);
613 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]);
615 SG_LOG(SG_FLIGHT,SG_INFO,"mass: " << mass );
616 SG_LOG(SG_FLIGHT,SG_INFO,"i_xx: " << i_xx );
617 SG_LOG(SG_FLIGHT,SG_INFO,"i_yy: " << i_yy );
618 SG_LOG(SG_FLIGHT,SG_INFO,"i_zz: " << i_zz );
619 SG_LOG(SG_FLIGHT,SG_INFO,"i_xz: " << i_xz );
620 SG_LOG(SG_FLIGHT,SG_INFO,"nlf: " << nlf );
621 SG_LOG(SG_FLIGHT,SG_INFO,"v_rel_wind: " << v_rel_wind );
622 SG_LOG(SG_FLIGHT,SG_INFO,"v_true_kts: " << v_true_kts );
623 SG_LOG(SG_FLIGHT,SG_INFO,"v_rel_ground: " << v_rel_ground );
624 SG_LOG(SG_FLIGHT,SG_INFO,"v_inertial: " << v_inertial );
625 SG_LOG(SG_FLIGHT,SG_INFO,"v_ground_speed: " << v_ground_speed );
626 SG_LOG(SG_FLIGHT,SG_INFO,"v_equiv: " << v_equiv );
627 SG_LOG(SG_FLIGHT,SG_INFO,"v_equiv_kts: " << v_equiv_kts );
628 SG_LOG(SG_FLIGHT,SG_INFO,"v_calibrated: " << v_calibrated );
629 SG_LOG(SG_FLIGHT,SG_INFO,"v_calibrated_kts: " << v_calibrated_kts );
630 SG_LOG(SG_FLIGHT,SG_INFO,"gravity: " << gravity );
631 SG_LOG(SG_FLIGHT,SG_INFO,"centrifugal_relief: " << centrifugal_relief );
632 SG_LOG(SG_FLIGHT,SG_INFO,"alpha: " << alpha );
633 SG_LOG(SG_FLIGHT,SG_INFO,"beta: " << beta );
634 SG_LOG(SG_FLIGHT,SG_INFO,"alpha_dot: " << alpha_dot );
635 SG_LOG(SG_FLIGHT,SG_INFO,"beta_dot: " << beta_dot );
636 SG_LOG(SG_FLIGHT,SG_INFO,"cos_alpha: " << cos_alpha );
637 SG_LOG(SG_FLIGHT,SG_INFO,"sin_alpha: " << sin_alpha );
638 SG_LOG(SG_FLIGHT,SG_INFO,"cos_beta: " << cos_beta );
639 SG_LOG(SG_FLIGHT,SG_INFO,"sin_beta: " << sin_beta );
640 SG_LOG(SG_FLIGHT,SG_INFO,"cos_phi: " << cos_phi );
641 SG_LOG(SG_FLIGHT,SG_INFO,"sin_phi: " << sin_phi );
642 SG_LOG(SG_FLIGHT,SG_INFO,"cos_theta: " << cos_theta );
643 SG_LOG(SG_FLIGHT,SG_INFO,"sin_theta: " << sin_theta );
644 SG_LOG(SG_FLIGHT,SG_INFO,"cos_psi: " << cos_psi );
645 SG_LOG(SG_FLIGHT,SG_INFO,"sin_psi: " << sin_psi );
646 SG_LOG(SG_FLIGHT,SG_INFO,"gamma_vert_rad: " << gamma_vert_rad );
647 SG_LOG(SG_FLIGHT,SG_INFO,"gamma_horiz_rad: " << gamma_horiz_rad );
648 SG_LOG(SG_FLIGHT,SG_INFO,"sigma: " << sigma );
649 SG_LOG(SG_FLIGHT,SG_INFO,"density: " << density );
650 SG_LOG(SG_FLIGHT,SG_INFO,"v_sound: " << v_sound );
651 SG_LOG(SG_FLIGHT,SG_INFO,"mach_number: " << mach_number );
652 SG_LOG(SG_FLIGHT,SG_INFO,"static_pressure: " << static_pressure );
653 SG_LOG(SG_FLIGHT,SG_INFO,"total_pressure: " << total_pressure );
654 SG_LOG(SG_FLIGHT,SG_INFO,"impact_pressure: " << impact_pressure );
655 SG_LOG(SG_FLIGHT,SG_INFO,"dynamic_pressure: " << dynamic_pressure );
656 SG_LOG(SG_FLIGHT,SG_INFO,"static_temperature: " << static_temperature );
657 SG_LOG(SG_FLIGHT,SG_INFO,"total_temperature: " << total_temperature );
658 SG_LOG(SG_FLIGHT,SG_INFO,"sea_level_radius: " << sea_level_radius );
659 SG_LOG(SG_FLIGHT,SG_INFO,"earth_position_angle: " << earth_position_angle );
660 SG_LOG(SG_FLIGHT,SG_INFO,"runway_altitude: " << runway_altitude );
661 SG_LOG(SG_FLIGHT,SG_INFO,"runway_latitude: " << runway_latitude );
662 SG_LOG(SG_FLIGHT,SG_INFO,"runway_longitude: " << runway_longitude );
663 SG_LOG(SG_FLIGHT,SG_INFO,"runway_heading: " << runway_heading );
664 SG_LOG(SG_FLIGHT,SG_INFO,"radius_to_rwy: " << radius_to_rwy );
665 SG_LOG(SG_FLIGHT,SG_INFO,"climb_rate: " << climb_rate );
666 SG_LOG(SG_FLIGHT,SG_INFO,"sin_lat_geocentric: " << sin_lat_geocentric );
667 SG_LOG(SG_FLIGHT,SG_INFO,"cos_lat_geocentric: " << cos_lat_geocentric );
668 SG_LOG(SG_FLIGHT,SG_INFO,"sin_longitude: " << sin_longitude );
669 SG_LOG(SG_FLIGHT,SG_INFO,"cos_longitude: " << cos_longitude );
670 SG_LOG(SG_FLIGHT,SG_INFO,"sin_latitude: " << sin_latitude );
671 SG_LOG(SG_FLIGHT,SG_INFO,"cos_latitude: " << cos_latitude );
672 SG_LOG(SG_FLIGHT,SG_INFO,"altitude_agl: " << altitude_agl );
676 void fgToggleFDMdataLogging(void) {
677 cur_fdm_state->ToggleDataLogging();