1 // flight.cxx -- 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.
28 #include <simgear/constants.h>
29 #include <simgear/debug/logstream.hxx>
30 #include <simgear/math/sg_geodesy.hxx>
31 #include <simgear/timing/timestamp.hxx>
33 #include <Scenery/scenery.hxx>
34 #include <FDM/LaRCsim/ls_interface.h>
35 #include <Main/globals.hxx>
36 #include <Main/fg_props.hxx>
37 #include <Main/location.hxx>
38 #include <Model/model.hxx>
39 #include <Model/acmodel.hxx>
44 // base_fdm_state is the internal state that is updated in integer
45 // multiples of "dt". This leads to "jitter" with respect to the real
46 // world time, so we introduce cur_fdm_state which is extrapolated by
47 // the difference between sim time and real world time
49 FGInterface *cur_fdm_state = 0;
50 FGInterface base_fdm_state;
52 inline void init_vec(FG_VECTOR_3 vec) {
53 vec[0] = 0.0; vec[1] = 0.0; vec[2] = 0.0;
57 FGInterface::FGInterface()
63 FGInterface::FGInterface( double dt )
70 FGInterface::~FGInterface() {
71 // unbind(); // FIXME: should be called explicitly
76 FGInterface::_calc_multiloop (double dt)
78 int hz = fgGetInt("/sim/model-hz");
79 int speedup = fgGetInt("/sim/speed-up");
84 int multiloop = int(floor(ml));
85 remainder = (ml - multiloop) / hz;
86 return (multiloop * speedup);
91 * Set default values for the state of the FDM.
93 * This method is invoked by the constructors.
96 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 FGInterface::init () {}
173 * Initialize the state of the FDM.
175 * Subclasses of FGInterface may do their own, additional initialization,
176 * but there is some that is common to all. Normally, they should call
177 * this before they begin their own init to make sure the basic structures
178 * are set up properly.
181 FGInterface::common_init ()
183 SG_LOG( SG_FLIGHT, SG_INFO, "Start common FDM init" );
188 // set_remainder( 0 );
190 // linking in FGAircraft instance...
191 // FIXME: when using multiple instances, then there will be more than
192 // one model so get_aircraft_model will have to be indexed to the correct
194 _acmodel = globals->get_aircraft_model();
196 // Set initial position
197 SG_LOG( SG_FLIGHT, SG_INFO, "...initializing position..." );
198 set_Longitude( fgGetDouble("/sim/presets/longitude-deg")
199 * SGD_DEGREES_TO_RADIANS );
200 set_Latitude( fgGetDouble("/sim/presets/latitude-deg")
201 * SGD_DEGREES_TO_RADIANS );
202 double ground_elev_m = globals->get_scenery()->get_cur_elev();
203 double ground_elev_ft = ground_elev_m * SG_METER_TO_FEET;
204 _acmodel->get3DModel()->getFGLocation()->set_cur_elev_m( ground_elev_m );
205 _set_Runway_altitude ( ground_elev_ft );
206 if ( fgGetBool("/sim/presets/onground")
207 || fgGetDouble("/sim/presets/altitude-ft") < ground_elev_ft ) {
208 fgSetDouble("/sim/presets/altitude-ft", ground_elev_ft);
209 fgSetDouble("/position/altitude-ft", ground_elev_ft);
211 set_Altitude( fgGetDouble("/sim/presets/altitude-ft") );
213 // Set ground elevation
214 SG_LOG( SG_FLIGHT, SG_INFO,
215 "...initializing ground elevation to " << ground_elev_ft
218 // Set sea-level radius
219 SG_LOG( SG_FLIGHT, SG_INFO, "...initializing sea-level radius..." );
220 SG_LOG( SG_FLIGHT, SG_INFO, " lat = "
221 << fgGetDouble("/sim/presets/latitude-deg")
222 << " alt = " << fgGetDouble("/sim/presets/altitude-ft") );
223 double sea_level_radius_meters;
225 sgGeodToGeoc( fgGetDouble("/sim/presets/latitude-deg")
226 * SGD_DEGREES_TO_RADIANS,
227 fgGetDouble("/sim/presets/altitude-ft") * SG_FEET_TO_METER,
228 &sea_level_radius_meters, &lat_geoc );
229 _set_Sea_level_radius( sea_level_radius_meters * SG_METER_TO_FEET );
231 // Set initial velocities
232 SG_LOG( SG_FLIGHT, SG_INFO, "...initializing velocities..." );
233 if ( !fgHasNode("/sim/presets/speed-set") ) {
234 set_V_calibrated_kts(0.0);
236 const string speedset = fgGetString("/sim/presets/speed-set");
237 if ( speedset == "knots" || speedset == "KNOTS" ) {
238 set_V_calibrated_kts( fgGetDouble("/sim/presets/airspeed-kt") );
239 } else if ( speedset == "mach" || speedset == "MACH" ) {
240 set_Mach_number( fgGetDouble("/sim/presets/mach") );
241 } else if ( speedset == "UVW" || speedset == "uvw" ) {
242 set_Velocities_Wind_Body(
243 fgGetDouble("/sim/presets/uBody-fps"),
244 fgGetDouble("/sim/presets/vBody-fps"),
245 fgGetDouble("/sim/presets/wBody-fps") );
246 } else if ( speedset == "NED" || speedset == "ned" ) {
247 set_Velocities_Local(
248 fgGetDouble("/sim/presets/speed-north-fps"),
249 fgGetDouble("/sim/presets/speed-east-fps"),
250 fgGetDouble("/sim/presets/speed-down-fps") );
252 SG_LOG( SG_FLIGHT, SG_ALERT,
253 "Unrecognized value for /sim/presets/speed-set: "
255 set_V_calibrated_kts( 0.0 );
259 // Set initial Euler angles
260 SG_LOG( SG_FLIGHT, SG_INFO, "...initializing Euler angles..." );
261 set_Euler_Angles( fgGetDouble("/sim/presets/roll-deg")
262 * SGD_DEGREES_TO_RADIANS,
263 fgGetDouble("/sim/presets/pitch-deg")
264 * SGD_DEGREES_TO_RADIANS,
265 fgGetDouble("/sim/presets/heading-deg")
266 * SGD_DEGREES_TO_RADIANS );
268 SG_LOG( SG_FLIGHT, SG_INFO, "End common FDM init" );
273 * Bind getters and setters to properties.
275 * The bind() method will be invoked after init(). Note that unlike
276 * the usual implementations of FGSubsystem::bind(), this method does
277 * not automatically pick up existing values for the properties at
278 * bind time; instead, all values are set explicitly in the init()
286 // Time management (read-only)
287 // fgTie("/fdm/time/delta_t", this,
288 // &FGInterface::get_delta_t); // read-only
289 // fgTie("/fdm/time/elapsed", this,
290 // &FGInterface::get_elapsed); // read-only
291 // fgTie("/fdm/time/remainder", this,
292 // &FGInterface::get_remainder); // read-only
293 // fgTie("/fdm/time/multi_loop", this,
294 // &FGInterface::get_multi_loop); // read-only
297 fgTie("/position/latitude-deg", this,
298 &FGInterface::get_Latitude_deg,
299 &FGInterface::set_Latitude_deg,
301 fgSetArchivable("/position/latitude-deg");
302 fgTie("/position/longitude-deg", this,
303 &FGInterface::get_Longitude_deg,
304 &FGInterface::set_Longitude_deg,
306 fgSetArchivable("/position/longitude-deg");
307 fgTie("/position/altitude-ft", this,
308 &FGInterface::get_Altitude,
309 &FGInterface::set_Altitude,
311 fgSetArchivable("/position/altitude-ft");
312 fgTie("/position/altitude-agl-ft", this,
313 &FGInterface::get_Altitude_AGL); // read-only
316 fgTie("/orientation/roll-deg", this,
317 &FGInterface::get_Phi_deg,
318 &FGInterface::set_Phi_deg);
319 fgSetArchivable("/orientation/roll-deg");
320 fgTie("/orientation/pitch-deg", this,
321 &FGInterface::get_Theta_deg,
322 &FGInterface::set_Theta_deg);
323 fgSetArchivable("/orientation/pitch-deg");
324 fgTie("/orientation/heading-deg", this,
325 &FGInterface::get_Psi_deg,
326 &FGInterface::set_Psi_deg);
327 fgSetArchivable("/orientation/heading-deg");
329 // Body-axis "euler rates" (rotation speed, but in a funny
331 fgTie("/orientation/roll-rate-degps", this,
332 &FGInterface::get_Phi_dot_degps);
333 fgTie("/orientation/pitch-rate-degps", this,
334 &FGInterface::get_Theta_dot_degps);
335 fgTie("/orientation/yaw-rate-degps", this,
336 &FGInterface::get_Psi_dot_degps);
338 // Calibrated airspeed
339 fgTie("/velocities/airspeed-kt", this,
340 &FGInterface::get_V_calibrated_kts,
341 &FGInterface::set_V_calibrated_kts,
345 // fgTie("/velocities/speed-north-fps", this,
346 // &FGInterface::get_V_north,
347 // &FGInterface::set_V_north);
348 // fgSetArchivable("/velocities/speed-north-fps");
349 // fgTie("/velocities/speed-east-fps", this,
350 // &FGInterface::get_V_east,
351 // &FGInterface::set_V_east);
352 // fgSetArchivable("/velocities/speed-east-fps");
353 // fgTie("/velocities/speed-down-fps", this,
354 // &FGInterface::get_V_down,
355 // &FGInterface::set_V_down);
356 // fgSetArchivable("/velocities/speed-down-fps");
357 // FIXME: Temporarily read-only, until the
358 // incompatibilities between JSBSim and
359 // LaRCSim are fixed (LaRCSim adds the
360 // earth's rotation to the east velocity).
361 fgTie("/velocities/speed-north-fps", this,
362 &FGInterface::get_V_north);
363 fgTie("/velocities/speed-east-fps", this,
364 &FGInterface::get_V_east);
365 fgTie("/velocities/speed-down-fps", this,
366 &FGInterface::get_V_down);
369 // FIXME: temporarily archivable, until
370 // the NED problem is fixed.
371 fgTie("/velocities/uBody-fps", this,
372 &FGInterface::get_uBody,
373 &FGInterface::set_uBody,
375 fgSetArchivable("/velocities/uBody-fps");
376 fgTie("/velocities/vBody-fps", this,
377 &FGInterface::get_vBody,
378 &FGInterface::set_vBody,
380 fgSetArchivable("/velocities/vBody-fps");
381 fgTie("/velocities/wBody-fps", this,
382 &FGInterface::get_wBody,
383 &FGInterface::set_wBody,
385 fgSetArchivable("/velocities/wBody-fps");
387 // Climb and slip (read-only)
388 fgTie("/velocities/vertical-speed-fps", this,
389 &FGInterface::get_Climb_Rate,
390 &FGInterface::set_Climb_Rate );
391 fgTie("/velocities/glideslope", this,
392 &FGInterface::get_Gamma_vert_rad,
393 &FGInterface::set_Gamma_vert_rad );
394 fgTie("/velocities/side-slip-rad", this,
395 &FGInterface::get_Beta); // read-only
396 fgTie("/velocities/side-slip-deg", this,
397 &FGInterface::get_Beta_deg); // read-only
398 fgTie("/velocities/alpha-deg", this,
399 &FGInterface::get_Alpha_deg); // read-only
400 fgTie("/accelerations/nlf", this,
401 &FGInterface::get_Nlf); // read-only
406 * Unbind any properties bound to this FDM.
408 * This method allows the FDM to release properties so that a new
409 * FDM can bind them instead.
412 FGInterface::unbind ()
416 fgUntie("/fdm/time/delta_t");
417 fgUntie("/fdm/time/elapsed");
418 fgUntie("/fdm/time/remainder");
419 fgUntie("/fdm/time/multi_loop");
420 fgUntie("/position/latitude-deg");
421 fgUntie("/position/longitude-deg");
422 fgUntie("/position/altitude-ft");
423 fgUntie("/position/altitude-agl-ft");
424 fgUntie("/orientation/heading-deg");
425 fgUntie("/orientation/pitch-deg");
426 fgUntie("/orientation/roll-deg");
427 fgUntie("/velocities/airspeed-kt");
428 fgUntie("/velocities/speed-north-fps");
429 fgUntie("/velocities/speed-east-fps");
430 fgUntie("/velocities/speed-down-fps");
431 fgUntie("/velocities/uBody-fps");
432 fgUntie("/velocities/vBody-fps");
433 fgUntie("/velocities/wBody-fps");
434 fgUntie("/velocities/vertical-speed-fps");
435 fgUntie("/velocities/glideslope");
436 fgUntie("/velocities/side-slip-rad");
437 fgUntie("/velocities/side-slip-deg");
438 fgUntie("/velocities/alpha-deg");
439 fgUntie("/accelerations/nlf");
444 * Update the state of the FDM (i.e. run the equations of motion).
447 FGInterface::update (double dt)
449 SG_LOG(SG_FLIGHT, SG_ALERT, "dummy update() ... SHOULDN'T BE CALLED!");
453 void FGInterface::_updateGeodeticPosition( double lat, double lon, double alt )
455 double lat_geoc, sl_radius;
457 // cout << "starting sea level rad = " << get_Sea_level_radius() << endl;
459 sgGeodToGeoc( lat, alt * SG_FEET_TO_METER, &sl_radius, &lat_geoc );
461 SG_LOG( SG_FLIGHT, SG_DEBUG, "lon = " << lon
462 << " lat_geod = " << lat
463 << " lat_geoc = " << lat_geoc
465 << " sl_radius = " << sl_radius * SG_METER_TO_FEET
466 << " Equator = " << SG_EQUATORIAL_RADIUS_FT );
468 _set_Geocentric_Position( lat_geoc, lon,
469 sl_radius * SG_METER_TO_FEET + alt );
471 _set_Geodetic_Position( lat, lon, alt );
473 _set_Sea_level_radius( sl_radius * SG_METER_TO_FEET );
474 _set_Runway_altitude( getACModel()->get3DModel()->getFGLocation()->get_cur_elev_m() * SG_METER_TO_FEET );
476 _set_sin_lat_geocentric( lat_geoc );
477 _set_cos_lat_geocentric( lat_geoc );
479 _set_sin_cos_longitude( lon );
481 _set_sin_cos_latitude( lat );
483 /* Norman's code for slope of the terrain */
484 /* needs to be tested -- get it on the HUD and taxi around */
485 /* double *tnorm = scenery.cur_normal;
487 double sy = sin ( -get_Psi() ) ;
488 double cy = cos ( -get_Psi() ) ;
490 double phitb, thetatb, psitb;
491 if ( tnorm[1] != 0.0 ) {
492 psitb = -atan2 ( tnorm[0], tnorm[1] );
494 if ( tnorm[2] != 0.0 ) {
495 thetatb = atan2 ( tnorm[0] * cy - tnorm[1] * sy, tnorm[2] );
496 phitb = -atan2 ( tnorm[1] * cy + tnorm[0] * sy, tnorm[2] );
499 _set_terrain_slope(phitb, thetatb, psitb)
504 void FGInterface::_updateGeocentricPosition( double lat_geoc, double lon,
507 double lat_geod, tmp_alt, sl_radius1, sl_radius2, tmp_lat_geoc;
509 // cout << "starting sea level rad = " << get_Sea_level_radius() << endl;
511 sgGeocToGeod( lat_geoc, ( get_Sea_level_radius() + alt ) * SG_FEET_TO_METER,
512 &lat_geod, &tmp_alt, &sl_radius1 );
513 sgGeodToGeoc( lat_geod, alt * SG_FEET_TO_METER, &sl_radius2, &tmp_lat_geoc );
515 SG_LOG( SG_FLIGHT, SG_DEBUG, "lon = " << lon
516 << " lat_geod = " << lat_geod
517 << " lat_geoc = " << lat_geoc
519 << " tmp_alt = " << tmp_alt * SG_METER_TO_FEET
520 << " sl_radius1 = " << sl_radius1 * SG_METER_TO_FEET
521 << " sl_radius2 = " << sl_radius2 * SG_METER_TO_FEET
522 << " Equator = " << SG_EQUATORIAL_RADIUS_FT );
524 _set_Geocentric_Position( lat_geoc, lon,
525 sl_radius2 * SG_METER_TO_FEET + alt );
527 _set_Geodetic_Position( lat_geod, lon, alt );
529 _set_Sea_level_radius( sl_radius2 * SG_METER_TO_FEET );
530 _set_Runway_altitude( getACModel()->get3DModel()->getFGLocation()->get_cur_elev_m() * SG_METER_TO_FEET );
532 _set_sin_lat_geocentric( lat_geoc );
533 _set_cos_lat_geocentric( lat_geoc );
535 _set_sin_cos_longitude( lon );
537 _set_sin_cos_latitude( lat_geod );
539 /* Norman's code for slope of the terrain */
540 /* needs to be tested -- get it on the HUD and taxi around */
541 /* double *tnorm = scenery.cur_normal;
543 double sy = sin ( -get_Psi() ) ;
544 double cy = cos ( -get_Psi() ) ;
546 double phitb, thetatb, psitb;
547 if ( tnorm[1] != 0.0 ) {
548 psitb = -atan2 ( tnorm[0], tnorm[1] );
550 if ( tnorm[2] != 0.0 ) {
551 thetatb = atan2 ( tnorm[0] * cy - tnorm[1] * sy, tnorm[2] );
552 phitb = -atan2 ( tnorm[1] * cy + tnorm[0] * sy, tnorm[2] );
555 _set_terrain_slope(phitb, thetatb, psitb)
560 // Extrapolate fdm based on time_offset (in usec)
561 void FGInterface::extrapolate( int time_offset ) {
562 double dt = time_offset / 1000000.0;
564 // -dw- metrowerks complains about ambiguous access, not critical
567 SG_LOG(SG_FLIGHT, SG_INFO, "extrapolating FDM by dt = " << dt);
570 double lat = geodetic_position_v[0] + geocentric_rates_v[0] * dt;
571 double lat_geoc = geocentric_position_v[0] + geocentric_rates_v[0] * dt;
573 double lon = geodetic_position_v[1] + geocentric_rates_v[1] * dt;
574 double lon_geoc = geocentric_position_v[1] + geocentric_rates_v[1] * dt;
576 double alt = geodetic_position_v[2] + geocentric_rates_v[2] * dt;
577 double radius = geocentric_position_v[2] + geocentric_rates_v[2] * dt;
579 geodetic_position_v[0] = lat;
580 geocentric_position_v[0] = lat_geoc;
582 geodetic_position_v[1] = lon;
583 geocentric_position_v[1] = lon_geoc;
585 geodetic_position_v[2] = alt;
586 geocentric_position_v[2] = radius;
590 void FGInterface::set_Latitude(double lat) {
591 geodetic_position_v[0] = lat;
594 void FGInterface::set_Longitude(double lon) {
595 geodetic_position_v[1] = lon;
598 void FGInterface::set_Altitude(double alt) {
599 geodetic_position_v[2] = alt;
602 void FGInterface::set_AltitudeAGL(double altagl) {
607 void FGInterface::set_V_calibrated_kts(double vc) {
608 v_calibrated_kts = vc;
611 void FGInterface::set_Mach_number(double mach) {
615 void FGInterface::set_Velocities_Local( double north,
618 v_local_v[0] = north;
623 void FGInterface::set_Velocities_Wind_Body( double u,
626 v_wind_body_v[0] = u;
627 v_wind_body_v[1] = v;
628 v_wind_body_v[2] = w;
632 void FGInterface::set_Euler_Angles( double phi,
635 euler_angles_v[0] = phi;
636 euler_angles_v[1] = theta;
637 euler_angles_v[2] = psi;
641 void FGInterface::set_Climb_Rate( double roc) {
645 void FGInterface::set_Gamma_vert_rad( double gamma) {
646 gamma_vert_rad = gamma;
649 void FGInterface::set_Static_pressure(double p) { static_pressure = p; }
650 void FGInterface::set_Static_temperature(double T) { static_temperature = T; }
651 void FGInterface::set_Density(double rho) { density = rho; }
653 void FGInterface::set_Velocities_Local_Airmass (double wnorth,
656 v_local_airmass_v[0] = wnorth;
657 v_local_airmass_v[1] = weast;
658 v_local_airmass_v[2] = wdown;
662 void FGInterface::_busdump(void) {
664 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]);
665 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]);
666 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]);
667 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]);
668 SG_LOG(SG_FLIGHT,SG_INFO,"f_aero_v[3]: " << f_aero_v[0] << ", " << f_aero_v[1] << ", " << f_aero_v[2]);
669 SG_LOG(SG_FLIGHT,SG_INFO,"f_engine_v[3]: " << f_engine_v[0] << ", " << f_engine_v[1] << ", " << f_engine_v[2]);
670 SG_LOG(SG_FLIGHT,SG_INFO,"f_gear_v[3]: " << f_gear_v[0] << ", " << f_gear_v[1] << ", " << f_gear_v[2]);
671 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]);
672 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]);
673 SG_LOG(SG_FLIGHT,SG_INFO,"m_aero_v[3]: " << m_aero_v[0] << ", " << m_aero_v[1] << ", " << m_aero_v[2]);
674 SG_LOG(SG_FLIGHT,SG_INFO,"m_engine_v[3]: " << m_engine_v[0] << ", " << m_engine_v[1] << ", " << m_engine_v[2]);
675 SG_LOG(SG_FLIGHT,SG_INFO,"m_gear_v[3]: " << m_gear_v[0] << ", " << m_gear_v[1] << ", " << m_gear_v[2]);
676 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]);
677 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]);
678 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]);
679 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]);
680 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]);
681 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]);
682 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]);
683 SG_LOG(SG_FLIGHT,SG_INFO,"v_local_v[3]: " << v_local_v[0] << ", " << v_local_v[1] << ", " << v_local_v[2]);
684 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]);
685 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]);
686 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]);
687 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]);
688 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]);
689 SG_LOG(SG_FLIGHT,SG_INFO,"omega_body_v[3]: " << omega_body_v[0] << ", " << omega_body_v[1] << ", " << omega_body_v[2]);
690 SG_LOG(SG_FLIGHT,SG_INFO,"omega_local_v[3]: " << omega_local_v[0] << ", " << omega_local_v[1] << ", " << omega_local_v[2]);
691 SG_LOG(SG_FLIGHT,SG_INFO,"omega_total_v[3]: " << omega_total_v[0] << ", " << omega_total_v[1] << ", " << omega_total_v[2]);
692 SG_LOG(SG_FLIGHT,SG_INFO,"euler_rates_v[3]: " << euler_rates_v[0] << ", " << euler_rates_v[1] << ", " << euler_rates_v[2]);
693 SG_LOG(SG_FLIGHT,SG_INFO,"geocentric_rates_v[3]: " << geocentric_rates_v[0] << ", " << geocentric_rates_v[1] << ", " << geocentric_rates_v[2]);
694 SG_LOG(SG_FLIGHT,SG_INFO,"geocentric_position_v[3]: " << geocentric_position_v[0] << ", " << geocentric_position_v[1] << ", " << geocentric_position_v[2]);
695 SG_LOG(SG_FLIGHT,SG_INFO,"geodetic_position_v[3]: " << geodetic_position_v[0] << ", " << geodetic_position_v[1] << ", " << geodetic_position_v[2]);
696 SG_LOG(SG_FLIGHT,SG_INFO,"euler_angles_v[3]: " << euler_angles_v[0] << ", " << euler_angles_v[1] << ", " << euler_angles_v[2]);
697 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]);
698 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]);
699 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]);
700 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]);
702 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]);
703 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]);
704 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]);
706 SG_LOG(SG_FLIGHT,SG_INFO,"mass: " << mass );
707 SG_LOG(SG_FLIGHT,SG_INFO,"i_xx: " << i_xx );
708 SG_LOG(SG_FLIGHT,SG_INFO,"i_yy: " << i_yy );
709 SG_LOG(SG_FLIGHT,SG_INFO,"i_zz: " << i_zz );
710 SG_LOG(SG_FLIGHT,SG_INFO,"i_xz: " << i_xz );
711 SG_LOG(SG_FLIGHT,SG_INFO,"nlf: " << nlf );
712 SG_LOG(SG_FLIGHT,SG_INFO,"v_rel_wind: " << v_rel_wind );
713 SG_LOG(SG_FLIGHT,SG_INFO,"v_true_kts: " << v_true_kts );
714 SG_LOG(SG_FLIGHT,SG_INFO,"v_rel_ground: " << v_rel_ground );
715 SG_LOG(SG_FLIGHT,SG_INFO,"v_inertial: " << v_inertial );
716 SG_LOG(SG_FLIGHT,SG_INFO,"v_ground_speed: " << v_ground_speed );
717 SG_LOG(SG_FLIGHT,SG_INFO,"v_equiv: " << v_equiv );
718 SG_LOG(SG_FLIGHT,SG_INFO,"v_equiv_kts: " << v_equiv_kts );
719 SG_LOG(SG_FLIGHT,SG_INFO,"v_calibrated: " << v_calibrated );
720 SG_LOG(SG_FLIGHT,SG_INFO,"v_calibrated_kts: " << v_calibrated_kts );
721 SG_LOG(SG_FLIGHT,SG_INFO,"gravity: " << gravity );
722 SG_LOG(SG_FLIGHT,SG_INFO,"centrifugal_relief: " << centrifugal_relief );
723 SG_LOG(SG_FLIGHT,SG_INFO,"alpha: " << alpha );
724 SG_LOG(SG_FLIGHT,SG_INFO,"beta: " << beta );
725 SG_LOG(SG_FLIGHT,SG_INFO,"alpha_dot: " << alpha_dot );
726 SG_LOG(SG_FLIGHT,SG_INFO,"beta_dot: " << beta_dot );
727 SG_LOG(SG_FLIGHT,SG_INFO,"cos_alpha: " << cos_alpha );
728 SG_LOG(SG_FLIGHT,SG_INFO,"sin_alpha: " << sin_alpha );
729 SG_LOG(SG_FLIGHT,SG_INFO,"cos_beta: " << cos_beta );
730 SG_LOG(SG_FLIGHT,SG_INFO,"sin_beta: " << sin_beta );
731 SG_LOG(SG_FLIGHT,SG_INFO,"cos_phi: " << cos_phi );
732 SG_LOG(SG_FLIGHT,SG_INFO,"sin_phi: " << sin_phi );
733 SG_LOG(SG_FLIGHT,SG_INFO,"cos_theta: " << cos_theta );
734 SG_LOG(SG_FLIGHT,SG_INFO,"sin_theta: " << sin_theta );
735 SG_LOG(SG_FLIGHT,SG_INFO,"cos_psi: " << cos_psi );
736 SG_LOG(SG_FLIGHT,SG_INFO,"sin_psi: " << sin_psi );
737 SG_LOG(SG_FLIGHT,SG_INFO,"gamma_vert_rad: " << gamma_vert_rad );
738 SG_LOG(SG_FLIGHT,SG_INFO,"gamma_horiz_rad: " << gamma_horiz_rad );
739 SG_LOG(SG_FLIGHT,SG_INFO,"sigma: " << sigma );
740 SG_LOG(SG_FLIGHT,SG_INFO,"density: " << density );
741 SG_LOG(SG_FLIGHT,SG_INFO,"v_sound: " << v_sound );
742 SG_LOG(SG_FLIGHT,SG_INFO,"mach_number: " << mach_number );
743 SG_LOG(SG_FLIGHT,SG_INFO,"static_pressure: " << static_pressure );
744 SG_LOG(SG_FLIGHT,SG_INFO,"total_pressure: " << total_pressure );
745 SG_LOG(SG_FLIGHT,SG_INFO,"impact_pressure: " << impact_pressure );
746 SG_LOG(SG_FLIGHT,SG_INFO,"dynamic_pressure: " << dynamic_pressure );
747 SG_LOG(SG_FLIGHT,SG_INFO,"static_temperature: " << static_temperature );
748 SG_LOG(SG_FLIGHT,SG_INFO,"total_temperature: " << total_temperature );
749 SG_LOG(SG_FLIGHT,SG_INFO,"sea_level_radius: " << sea_level_radius );
750 SG_LOG(SG_FLIGHT,SG_INFO,"earth_position_angle: " << earth_position_angle );
751 SG_LOG(SG_FLIGHT,SG_INFO,"runway_altitude: " << runway_altitude );
752 SG_LOG(SG_FLIGHT,SG_INFO,"runway_latitude: " << runway_latitude );
753 SG_LOG(SG_FLIGHT,SG_INFO,"runway_longitude: " << runway_longitude );
754 SG_LOG(SG_FLIGHT,SG_INFO,"runway_heading: " << runway_heading );
755 SG_LOG(SG_FLIGHT,SG_INFO,"radius_to_rwy: " << radius_to_rwy );
756 SG_LOG(SG_FLIGHT,SG_INFO,"climb_rate: " << climb_rate );
757 SG_LOG(SG_FLIGHT,SG_INFO,"sin_lat_geocentric: " << sin_lat_geocentric );
758 SG_LOG(SG_FLIGHT,SG_INFO,"cos_lat_geocentric: " << cos_lat_geocentric );
759 SG_LOG(SG_FLIGHT,SG_INFO,"sin_longitude: " << sin_longitude );
760 SG_LOG(SG_FLIGHT,SG_INFO,"cos_longitude: " << cos_longitude );
761 SG_LOG(SG_FLIGHT,SG_INFO,"sin_latitude: " << sin_latitude );
762 SG_LOG(SG_FLIGHT,SG_INFO,"cos_latitude: " << cos_latitude );
763 SG_LOG(SG_FLIGHT,SG_INFO,"altitude_agl: " << altitude_agl );
767 void fgToggleFDMdataLogging(void) {
768 cur_fdm_state->ToggleDataLogging();