1 // navradio.cxx -- class to manage a nav radio instance
3 // Written by Curtis Olson, started April 2000.
5 // Copyright (C) 2000 - 2002 Curtis L. Olson - http://www.flightgear.org/~curt
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., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
32 #include <simgear/compiler.h>
33 #include <simgear/sg_inlines.h>
34 #include <simgear/math/sg_random.h>
35 #include <simgear/math/vector.hxx>
36 #include <simgear/structure/exception.hxx>
38 #include <Aircraft/aircraft.hxx>
39 #include <Navaids/navlist.hxx>
41 #include "navradio.hxx"
48 FGNavRadio::FGNavRadio(SGPropertyNode *node) :
49 lon_node(fgGetNode("/position/longitude-deg", true)),
50 lat_node(fgGetNode("/position/latitude-deg", true)),
51 alt_node(fgGetNode("/position/altitude-ft", true)),
56 sel_radial_node(NULL),
60 backcourse_node(NULL),
61 nav_serviceable_node(NULL),
62 cdi_serviceable_node(NULL),
63 gs_serviceable_node(NULL),
64 tofrom_serviceable_node(NULL),
66 fmt_alt_freq_node(NULL),
69 recip_radial_node(NULL),
70 target_radial_true_node(NULL),
71 target_auto_hdg_node(NULL),
72 time_to_intercept(NULL),
76 cdi_deflection_node(NULL),
77 cdi_xtrack_error_node(NULL),
78 cdi_xtrack_hdg_err_node(NULL),
82 gs_deflection_node(NULL),
83 gs_rate_of_climb_node(NULL),
90 nav_slaved_to_gps_node(NULL),
91 gps_cdi_deflection_node(NULL),
92 gps_to_flag_node(NULL),
93 gps_from_flag_node(NULL),
103 last_xtrack_error(0.0),
104 _name(node->getStringValue("name", "nav")),
105 _num(node->getIntValue("number", 0)),
106 _time_before_search_sec(-1.0)
108 SGPath path( globals->get_fg_root() );
110 term.append( "Navaids/range.term" );
112 low.append( "Navaids/range.low" );
114 high.append( "Navaids/range.high" );
116 term_tbl = new SGInterpTable( term.str() );
117 low_tbl = new SGInterpTable( low.str() );
118 high_tbl = new SGInterpTable( high.str() );
123 FGNavRadio::~FGNavRadio()
137 branch = "/instrumentation/" + _name;
139 SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
142 fgGetNode(("/systems/electrical/outputs/" + _name).c_str(), true);
145 is_valid_node = node->getChild("data-is-valid", 0, true);
146 power_btn_node = node->getChild("power-btn", 0, true);
147 power_btn_node->setBoolValue( true );
148 vol_btn_node = node->getChild("volume", 0, true);
149 ident_btn_node = node->getChild("ident", 0, true);
150 ident_btn_node->setBoolValue( true );
151 audio_btn_node = node->getChild("audio-btn", 0, true);
152 audio_btn_node->setBoolValue( true );
153 backcourse_node = node->getChild("back-course-btn", 0, true);
154 backcourse_node->setBoolValue( false );
155 nav_serviceable_node = node->getChild("serviceable", 0, true);
156 cdi_serviceable_node = (node->getChild("cdi", 0, true))
157 ->getChild("serviceable", 0, true);
158 gs_serviceable_node = (node->getChild("gs", 0, true))
159 ->getChild("serviceable");
160 tofrom_serviceable_node = (node->getChild("to-from", 0, true))
161 ->getChild("serviceable", 0, true);
164 SGPropertyNode *subnode = node->getChild("frequencies", 0, true);
165 freq_node = subnode->getChild("selected-mhz", 0, true);
166 alt_freq_node = subnode->getChild("standby-mhz", 0, true);
167 fmt_freq_node = subnode->getChild("selected-mhz-fmt", 0, true);
168 fmt_alt_freq_node = subnode->getChild("standby-mhz-fmt", 0, true);
171 subnode = node->getChild("radials", 0, true);
172 sel_radial_node = subnode->getChild("selected-deg", 0, true);
173 radial_node = subnode->getChild("actual-deg", 0, true);
174 recip_radial_node = subnode->getChild("reciprocal-radial-deg", 0, true);
175 target_radial_true_node = subnode->getChild("target-radial-deg", 0, true);
176 target_auto_hdg_node = subnode->getChild("target-auto-hdg-deg", 0, true);
179 heading_node = node->getChild("heading-deg", 0, true);
180 time_to_intercept = node->getChild("time-to-intercept-sec", 0, true);
181 to_flag_node = node->getChild("to-flag", 0, true);
182 from_flag_node = node->getChild("from-flag", 0, true);
183 inrange_node = node->getChild("in-range", 0, true);
184 cdi_deflection_node = node->getChild("heading-needle-deflection", 0, true);
185 cdi_xtrack_error_node = node->getChild("crosstrack-error-m", 0, true);
186 cdi_xtrack_hdg_err_node
187 = node->getChild("crosstrack-heading-error-deg", 0, true);
188 has_gs_node = node->getChild("has-gs", 0, true);
189 loc_node = node->getChild("nav-loc", 0, true);
190 loc_dist_node = node->getChild("nav-distance", 0, true);
191 gs_deflection_node = node->getChild("gs-needle-deflection", 0, true);
192 gs_rate_of_climb_node = node->getChild("gs-rate-of-climb", 0, true);
193 gs_dist_node = node->getChild("gs-distance", 0, true);
194 nav_id_node = node->getChild("nav-id", 0, true);
195 id_c1_node = node->getChild("nav-id_asc1", 0, true);
196 id_c2_node = node->getChild("nav-id_asc2", 0, true);
197 id_c3_node = node->getChild("nav-id_asc3", 0, true);
198 id_c4_node = node->getChild("nav-id_asc4", 0, true);
200 // gps slaving support
201 nav_slaved_to_gps_node = node->getChild("slaved-to-gps", 0, true);
202 gps_cdi_deflection_node = fgGetNode("/instrumentation/gps/cdi-deflection", true);
203 gps_to_flag_node = fgGetNode("/instrumentation/gps/to-flag", true);
204 gps_from_flag_node = fgGetNode("/instrumentation/gps/from-flag", true);
206 std::ostringstream temp;
207 temp << _name << "nav-ident" << _num;
208 nav_fx_name = temp.str();
209 temp << _name << "dme-ident" << _num;
210 dme_fx_name = temp.str();
216 std::ostringstream temp;
219 branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
224 FGNavRadio::unbind ()
226 std::ostringstream temp;
229 branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
233 // model standard VOR/DME/TACAN service volumes as per AIM 1-1-8
234 double FGNavRadio::adjustNavRange( double stationElev, double aircraftElev,
235 double nominalRange )
237 // extend out actual usable range to be 1.3x the published safe range
238 const double usability_factor = 1.3;
240 // assumptions we model the standard service volume, plus
241 // ... rather than specifying a cylinder, we model a cone that
242 // contains the cylinder. Then we put an upside down cone on top
243 // to model diminishing returns at too-high altitudes.
245 // altitude difference
246 double alt = ( aircraftElev * SG_METER_TO_FEET - stationElev );
247 // cout << "aircraft elev = " << aircraftElev * SG_METER_TO_FEET
248 // << " station elev = " << stationElev << endl;
250 if ( nominalRange < 25.0 + SG_EPSILON ) {
251 // Standard Terminal Service Volume
252 return term_tbl->interpolate( alt ) * usability_factor;
253 } else if ( nominalRange < 50.0 + SG_EPSILON ) {
254 // Standard Low Altitude Service Volume
255 // table is based on range of 40, scale to actual range
256 return low_tbl->interpolate( alt ) * nominalRange / 40.0
259 // Standard High Altitude Service Volume
260 // table is based on range of 130, scale to actual range
261 return high_tbl->interpolate( alt ) * nominalRange / 130.0
267 // model standard ILS service volumes as per AIM 1-1-9
268 double FGNavRadio::adjustILSRange( double stationElev, double aircraftElev,
269 double offsetDegrees, double distance )
271 // assumptions we model the standard service volume, plus
273 // altitude difference
274 // double alt = ( aircraftElev * SG_METER_TO_FEET - stationElev );
275 // double offset = fabs( offsetDegrees );
277 // if ( offset < 10 ) {
278 // return FG_ILS_DEFAULT_RANGE;
279 // } else if ( offset < 35 ) {
280 // return 10 + (35 - offset) * (FG_ILS_DEFAULT_RANGE - 10) / 25;
281 // } else if ( offset < 45 ) {
282 // return (45 - offset);
283 // } else if ( offset > 170 ) {
284 // return FG_ILS_DEFAULT_RANGE;
285 // } else if ( offset > 145 ) {
286 // return 10 + (offset - 145) * (FG_ILS_DEFAULT_RANGE - 10) / 25;
287 // } else if ( offset > 135 ) {
288 // return (offset - 135);
292 return FG_LOC_DEFAULT_RANGE;
296 //////////////////////////////////////////////////////////////////////////
297 // Update the various nav values based on position and valid tuned in navs
298 //////////////////////////////////////////////////////////////////////////
300 FGNavRadio::update(double dt)
302 // Do a nav station search only once a second to reduce
303 // unnecessary work. (Also, make sure to do this before caching
305 _time_before_search_sec -= dt;
306 if ( _time_before_search_sec < 0 ) {
310 // cache a few strategic values locally for speed
311 SGGeod pos = SGGeod::fromDegFt(lon_node->getDoubleValue(),
312 lat_node->getDoubleValue(),
313 alt_node->getDoubleValue());
314 bool power_btn = power_btn_node->getBoolValue();
315 bool nav_serviceable = nav_serviceable_node->getBoolValue();
316 bool cdi_serviceable = cdi_serviceable_node->getBoolValue();
317 bool tofrom_serviceable = tofrom_serviceable_node->getBoolValue();
318 bool inrange = inrange_node->getBoolValue();
319 bool has_gs = has_gs_node->getBoolValue();
320 bool is_loc = loc_node->getBoolValue();
321 double loc_dist = loc_dist_node->getDoubleValue();
325 // Create "formatted" versions of the nav frequencies for
326 // instrument displays.
328 sprintf( tmp, "%.2f", freq_node->getDoubleValue() );
329 fmt_freq_node->setStringValue(tmp);
330 sprintf( tmp, "%.2f", alt_freq_node->getDoubleValue() );
331 fmt_alt_freq_node->setStringValue(tmp);
333 // cout << "is_valid = " << is_valid
334 // << " power_btn = " << power_btn
335 // << " bus_power = " << bus_power_node->getDoubleValue()
336 // << " nav_serviceable = " << nav_serviceable
339 if ( is_valid && power_btn && (bus_power_node->getDoubleValue() > 1.0)
342 SGVec3d aircraft = SGVec3d::fromGeod(pos);
343 loc_dist = dist(aircraft, nav_xyz);
344 loc_dist_node->setDoubleValue( loc_dist );
345 // cout << "dt = " << dt << " dist = " << loc_dist << endl;
348 // find closest distance to the gs base line
349 SGVec3d p = aircraft;
350 double dist = sgdClosestPointToLineDistSquared(p.sg(), gs_xyz.sg(),
352 gs_dist_node->setDoubleValue( sqrt( dist ) );
353 // cout << "gs_dist = " << gs_dist_node->getDoubleValue()
356 // wgs84 heading to glide slope (to determine sign of distance)
357 geo_inverse_wgs_84( pos, SGGeod::fromDeg(gs_lon, gs_lat),
359 double r = az1 - target_radial;
360 while ( r > 180.0 ) { r -= 360.0;}
361 while ( r < -180.0 ) { r += 360.0;}
362 if ( r >= -90.0 && r <= 90.0 ) {
363 gs_dist_signed = gs_dist_node->getDoubleValue();
365 gs_dist_signed = -gs_dist_node->getDoubleValue();
367 /* cout << "Target Radial = " << target_radial
368 << " Bearing = " << az1
369 << " dist (signed) = " << gs_dist_signed
373 gs_dist_node->setDoubleValue( 0.0 );
376 //////////////////////////////////////////////////////////
377 // compute forward and reverse wgs84 headings to localizer
378 //////////////////////////////////////////////////////////
380 geo_inverse_wgs_84( pos, SGGeod::fromDeg(loc_lon, loc_lat),
382 // cout << "az1 = " << az1 << " magvar = " << nav_magvar << endl;
383 heading_node->setDoubleValue( hdg );
384 radial = az2 - twist;
385 double recip = radial + 180.0;
386 if ( recip >= 360.0 ) { recip -= 360.0; }
387 radial_node->setDoubleValue( radial );
388 recip_radial_node->setDoubleValue( recip );
389 // cout << " heading = " << heading_node->getDoubleValue()
390 // << " dist = " << nav_dist << endl;
392 //////////////////////////////////////////////////////////
393 // compute the target/selected radial in "true" heading
394 //////////////////////////////////////////////////////////
397 // ILS localizers radials are already "true" in our
399 trtrue = target_radial;
401 // VOR radials need to have that vor's offset added in
402 trtrue = target_radial + twist;
405 while ( trtrue < 0.0 ) { trtrue += 360.0; }
406 while ( trtrue > 360.0 ) { trtrue -= 360.0; }
407 target_radial_true_node->setDoubleValue( trtrue );
409 //////////////////////////////////////////////////////////
410 // adjust reception range for altitude
411 // FIXME: make sure we are using the navdata range now that
412 // it is valid in the data file
413 //////////////////////////////////////////////////////////
415 double offset = radial - target_radial;
416 while ( offset < -180.0 ) { offset += 360.0; }
417 while ( offset > 180.0 ) { offset -= 360.0; }
418 // cout << "ils offset = " << offset << endl;
420 = adjustILSRange( nav_elev, pos.getElevationM(), offset,
421 loc_dist * SG_METER_TO_NM );
424 = adjustNavRange( nav_elev, pos.getElevationM(), range );
426 // cout << "nav range = " << effective_range
427 // << " (" << range << ")" << endl;
429 if ( loc_dist < effective_range * SG_NM_TO_METER ) {
431 } else if ( loc_dist < 2 * effective_range * SG_NM_TO_METER ) {
432 inrange = sg_random() < ( 2 * effective_range * SG_NM_TO_METER
434 / (effective_range * SG_NM_TO_METER);
438 inrange_node->setBoolValue( inrange );
441 target_radial = sel_radial_node->getDoubleValue();
444 //////////////////////////////////////////////////////////
445 // compute to/from flag status
446 //////////////////////////////////////////////////////////
448 double offset = fabs(radial - target_radial);
449 if ( tofrom_serviceable ) {
450 if ( nav_slaved_to_gps_node->getBoolValue() ) {
451 value = gps_to_flag_node->getBoolValue();
452 } else if ( inrange ) {
456 value = !(offset <= 90.0 || offset >= 270.0);
462 to_flag_node->setBoolValue( value );
465 if ( tofrom_serviceable ) {
466 if ( nav_slaved_to_gps_node->getBoolValue() ) {
467 value = gps_from_flag_node->getBoolValue();
468 } else if ( inrange ) {
472 value = !(offset > 90.0 && offset < 270.0);
478 from_flag_node->setBoolValue( value );
480 //////////////////////////////////////////////////////////
481 // compute the deflection of the CDI needle, clamped to the range
483 //////////////////////////////////////////////////////////
485 bool loc_backside = false; // an in-code flag indicating that we are
486 // on a localizer backcourse.
487 if ( cdi_serviceable ) {
488 if ( nav_slaved_to_gps_node->getBoolValue() ) {
489 r = gps_cdi_deflection_node->getDoubleValue();
490 // We want +- 5 dots deflection for the gps, so clamp
492 SG_CLAMP_RANGE( r, -12.5, 12.5 );
493 } else if ( inrange ) {
494 r = radial - target_radial;
495 // cout << "Target radial = " << target_radial
496 // << " Actual radial = " << radial << endl;
498 while ( r > 180.0 ) { r -= 360.0;}
499 while ( r < -180.0 ) { r += 360.0;}
500 if ( fabs(r) > 90.0 ) {
501 r = ( r<0.0 ? -r-180.0 : -r+180.0 );
508 r = -r; // reverse, since radial is outbound
510 // According to Robin Peel, the ILS is 4x more
511 // sensitive than a vor
514 SG_CLAMP_RANGE( r, -10.0, 10.0 );
517 cdi_deflection_node->setDoubleValue( r );
519 //////////////////////////////////////////////////////////
520 // compute the amount of cross track distance error in meters
521 //////////////////////////////////////////////////////////
522 double xtrack_error = 0.0;
523 if ( inrange && nav_serviceable && cdi_serviceable ) {
524 r = radial - target_radial;
525 // cout << "Target radial = " << target_radial
526 // << " Actual radial = " << radial
527 // << " r = " << r << endl;
529 while ( r > 180.0 ) { r -= 360.0;}
530 while ( r < -180.0 ) { r += 360.0;}
531 if ( fabs(r) > 90.0 ) {
532 r = ( r<0.0 ? -r-180.0 : -r+180.0 );
535 r = -r; // reverse, since radial is outbound
537 xtrack_error = loc_dist * sin(r * SGD_DEGREES_TO_RADIANS);
541 cdi_xtrack_error_node->setDoubleValue( xtrack_error );
543 //////////////////////////////////////////////////////////
544 // compute an approximate ground track heading error
545 //////////////////////////////////////////////////////////
546 double hdg_error = 0.0;
547 if ( inrange && cdi_serviceable ) {
548 double vn = fgGetDouble( "/velocities/speed-north-fps" );
549 double ve = fgGetDouble( "/velocities/speed-east-fps" );
550 double gnd_trk_true = atan2( ve, vn ) * SGD_RADIANS_TO_DEGREES;
551 if ( gnd_trk_true < 0.0 ) { gnd_trk_true += 360.0; }
553 SGPropertyNode *true_hdg
554 = fgGetNode("/orientation/heading-deg", true);
555 hdg_error = gnd_trk_true - true_hdg->getDoubleValue();
557 // cout << "ground track = " << gnd_trk_true
558 // << " orientation = " << true_hdg->getDoubleValue() << endl;
560 cdi_xtrack_hdg_err_node->setDoubleValue( hdg_error );
562 //////////////////////////////////////////////////////////
563 // compute the time to intercept selected radial (based on
564 // current and last cross track errors and dt
565 //////////////////////////////////////////////////////////
567 if ( inrange && cdi_serviceable ) {
568 double xrate_ms = (last_xtrack_error - xtrack_error) / dt;
569 if ( fabs(xrate_ms) > 0.00001 ) {
570 t = xtrack_error / xrate_ms;
575 time_to_intercept->setDoubleValue( t );
577 //////////////////////////////////////////////////////////
578 // compute the amount of glide slope needle deflection
579 // (.i.e. the number of degrees we are off the glide slope * 5.0
581 // CLO - 13 Mar 2006: The glide slope needle should peg at
582 // +/-0.7 degrees off the ideal glideslope. I'm not sure why
583 // we compute the factor the way we do (5*gs_error), but we
584 // need to compensate for our 'odd' number in the glideslope
585 // needle animation. This means that the needle should peg
586 // when this values is +/-3.5.
587 //////////////////////////////////////////////////////////
589 if ( has_gs && gs_serviceable_node->getBoolValue() ) {
590 if ( nav_slaved_to_gps_node->getBoolValue() ) {
591 // FIXME/FINISHME, what should be set here?
592 } else if ( inrange ) {
593 double x = gs_dist_node->getDoubleValue();
594 double y = (fgGetDouble("/position/altitude-ft") - nav_elev)
596 // cout << "dist = " << x << " height = " << y << endl;
597 double angle = asin( y / x ) * SGD_RADIANS_TO_DEGREES;
598 r = (target_gs - angle) * 5.0;
601 gs_deflection_node->setDoubleValue( r );
603 //////////////////////////////////////////////////////////
604 // Calculate desired rate of climb for intercepting the GS
605 //////////////////////////////////////////////////////////
606 double x = gs_dist_node->getDoubleValue();
607 double y = (alt_node->getDoubleValue() - nav_elev)
609 double current_angle = atan2( y, x ) * SGD_RADIANS_TO_DEGREES;
611 double target_angle = target_gs;
612 double gs_diff = target_angle - current_angle;
614 // convert desired vertical path angle into a climb rate
615 double des_angle = current_angle - 10 * gs_diff;
617 // estimate horizontal speed towards ILS in meters per minute
618 double dist = last_x - x;
622 double new_vel = ( dist / dt );
624 horiz_vel = 0.75 * horiz_vel + 0.25 * new_vel;
625 // double horiz_vel = cur_fdm_state->get_V_ground_speed()
626 // * SG_FEET_TO_METER * 60.0;
627 // double horiz_vel = airspeed_node->getFloatValue()
628 // * SG_FEET_TO_METER * 60.0;
630 gs_rate_of_climb_node
631 ->setDoubleValue( -sin( des_angle * SGD_DEGREES_TO_RADIANS )
632 * horiz_vel * SG_METER_TO_FEET );
635 //////////////////////////////////////////////////////////
636 // Calculate a suggested target heading to smoothly intercept
638 //////////////////////////////////////////////////////////
640 // Now that we have cross track heading adjustment built in,
641 // we shouldn't need to overdrive the heading angle within 8km
644 // The cdi deflection should be +/-10 for a full range of deflection
645 // so multiplying this by 3 gives us +/- 30 degrees heading
647 double adjustment = cdi_deflection_node->getDoubleValue() * 3.0;
648 SG_CLAMP_RANGE( adjustment, -30.0, 30.0 );
650 // determine the target heading to fly to intercept the
651 // tgt_radial = target radial (true) + cdi offset adjustmest -
652 // xtrack heading error adjustment
654 if ( is_loc && backcourse_node->getBoolValue() ) {
655 // tuned to a localizer and backcourse mode activated
656 trtrue += 180.0; // reverse the target localizer heading
657 while ( trtrue > 360.0 ) { trtrue -= 360.0; }
658 nta_hdg = trtrue - adjustment - hdg_error;
660 nta_hdg = trtrue + adjustment - hdg_error;
663 while ( nta_hdg < 0.0 ) { nta_hdg += 360.0; }
664 while ( nta_hdg >= 360.0 ) { nta_hdg -= 360.0; }
665 target_auto_hdg_node->setDoubleValue( nta_hdg );
667 last_xtrack_error = xtrack_error;
669 inrange_node->setBoolValue( false );
670 cdi_deflection_node->setDoubleValue( 0.0 );
671 cdi_xtrack_error_node->setDoubleValue( 0.0 );
672 cdi_xtrack_hdg_err_node->setDoubleValue( 0.0 );
673 time_to_intercept->setDoubleValue( 0.0 );
674 gs_deflection_node->setDoubleValue( 0.0 );
675 to_flag_node->setBoolValue( false );
676 from_flag_node->setBoolValue( false );
677 // cout << "not picking up vor. :-(" << endl;
681 if ( is_valid && inrange && nav_serviceable ) {
682 // play station ident via audio system if on + ident,
683 // otherwise turn it off
685 && (bus_power_node->getDoubleValue() > 1.0)
686 && ident_btn_node->getBoolValue()
687 && audio_btn_node->getBoolValue() )
689 SGSoundSample *sound;
690 sound = globals->get_soundmgr()->find( nav_fx_name );
691 double vol = vol_btn_node->getDoubleValue();
692 if ( vol < 0.0 ) { vol = 0.0; }
693 if ( vol > 1.0 ) { vol = 1.0; }
694 if ( sound != NULL ) {
695 sound->set_volume( vol );
697 SG_LOG( SG_COCKPIT, SG_ALERT,
698 "Can't find nav-vor-ident sound" );
700 sound = globals->get_soundmgr()->find( dme_fx_name );
701 if ( sound != NULL ) {
702 sound->set_volume( vol );
704 SG_LOG( SG_COCKPIT, SG_ALERT,
705 "Can't find nav-dme-ident sound" );
707 // cout << "last_time = " << last_time << " ";
708 // cout << "cur_time = "
709 // << globals->get_time_params()->get_cur_time();
711 globals->get_time_params()->get_cur_time() - 30 ) {
712 last_time = globals->get_time_params()->get_cur_time();
715 // cout << " play_count = " << play_count << endl;
716 // cout << "playing = "
717 // << globals->get_soundmgr()->is_playing(nav_fx_name)
719 if ( play_count < 4 ) {
721 if ( !globals->get_soundmgr()->is_playing(nav_fx_name) ) {
722 globals->get_soundmgr()->play_once( nav_fx_name );
725 } else if ( play_count < 5 && has_dme ) {
727 if ( !globals->get_soundmgr()->is_playing(nav_fx_name) &&
728 !globals->get_soundmgr()->is_playing(dme_fx_name) ) {
729 globals->get_soundmgr()->play_once( dme_fx_name );
734 globals->get_soundmgr()->stop( nav_fx_name );
735 globals->get_soundmgr()->stop( dme_fx_name );
739 last_loc_dist = loc_dist;
743 // Update current nav/adf radio stations based on current postition
744 void FGNavRadio::search()
748 _time_before_search_sec = 1.0;
750 // cache values locally for speed
751 double lon = lon_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
752 double lat = lat_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
753 double elev = alt_node->getDoubleValue() * SG_FEET_TO_METER;
755 FGNavRecord *nav = NULL;
756 FGNavRecord *loc = NULL;
757 FGNavRecord *dme = NULL;
758 FGNavRecord *gs = NULL;
760 ////////////////////////////////////////////////////////////////////////
762 ////////////////////////////////////////////////////////////////////////
764 double freq = freq_node->getDoubleValue();
765 nav = globals->get_navlist()->findByFreq(freq, lon, lat, elev);
766 dme = globals->get_dmelist()->findByFreq(freq, lon, lat, elev);
768 loc = globals->get_loclist()->findByFreq(freq, lon, lat, elev);
769 gs = globals->get_gslist()->findByFreq(freq, lon, lat, elev);
775 nav_id = loc->get_ident();
776 nav_id_node->setStringValue( nav_id.c_str() );
777 // cout << "localizer = " << nav_id_node->getStringValue() << endl;
779 if ( last_nav_id != nav_id || last_nav_vor ) {
780 trans_ident = loc->get_trans_ident();
781 target_radial = loc->get_multiuse();
782 while ( target_radial < 0.0 ) { target_radial += 360.0; }
783 while ( target_radial > 360.0 ) { target_radial -= 360.0; }
784 loc_lon = loc->get_lon();
785 loc_lat = loc->get_lat();
786 nav_xyz = loc->get_cart();
787 last_nav_id = nav_id;
788 last_nav_vor = false;
789 loc_node->setBoolValue( true );
790 has_dme = (dme != NULL);
792 has_gs_node->setBoolValue( true );
793 gs_lon = gs->get_lon();
794 gs_lat = gs->get_lat();
795 nav_elev = gs->get_elev_ft();
796 int tmp = (int)(gs->get_multiuse() / 1000.0);
797 target_gs = (double)tmp / 100.0;
798 gs_xyz = gs->get_cart();
800 // derive GS baseline (perpendicular to the runay
802 double tlon, tlat, taz;
803 geo_direct_wgs_84 ( 0.0, gs_lat, gs_lon,
805 100.0, &tlat, &tlon, &taz );
806 // cout << "target_radial = " << target_radial << endl;
807 // cout << "nav_loc = " << loc_node->getBoolValue() << endl;
808 // cout << gs_lon << "," << gs_lat << " "
809 // << tlon << "," << tlat << " (" << nav_elev << ")"
811 SGGeod tpos = SGGeod::fromDegFt(tlon, tlat, nav_elev);
812 SGVec3d p1 = SGVec3d::fromGeod(tpos);
814 // cout << gs_xyz << endl;
815 // cout << p1 << endl;
816 gs_base_vec = p1 - gs_xyz;
817 // cout << gs_base_vec << endl;
819 has_gs_node->setBoolValue( false );
820 nav_elev = loc->get_elev_ft();
823 range = FG_LOC_DEFAULT_RANGE;
824 effective_range = range;
826 if ( globals->get_soundmgr()->exists( nav_fx_name ) ) {
827 globals->get_soundmgr()->remove( nav_fx_name );
829 SGSoundSample *sound;
830 sound = morse.make_ident( trans_ident, LO_FREQUENCY );
831 sound->set_volume( 0.3 );
832 globals->get_soundmgr()->add( sound, nav_fx_name );
834 if ( globals->get_soundmgr()->exists( dme_fx_name ) ) {
835 globals->get_soundmgr()->remove( dme_fx_name );
837 sound = morse.make_ident( trans_ident, HI_FREQUENCY );
838 sound->set_volume( 0.3 );
839 globals->get_soundmgr()->add( sound, dme_fx_name );
841 int offset = (int)(sg_random() * 30.0);
842 play_count = offset / 4;
843 last_time = globals->get_time_params()->get_cur_time() -
845 // cout << "offset = " << offset << " play_count = "
847 // << " last_time = " << last_time
848 // << " current time = "
849 // << globals->get_time_params()->get_cur_time() << endl;
851 // cout << "Found an loc station in range" << endl;
852 // cout << " id = " << loc->get_locident() << endl;
854 } else if ( nav != NULL ) {
855 nav_id = nav->get_ident();
856 nav_id_node->setStringValue( nav_id.c_str() );
857 // cout << "nav = " << nav_id << endl;
859 if ( last_nav_id != nav_id || !last_nav_vor ) {
860 last_nav_id = nav_id;
862 trans_ident = nav->get_trans_ident();
863 loc_node->setBoolValue( false );
864 has_dme = (dme != NULL);
865 has_gs_node->setBoolValue( false );
866 loc_lon = nav->get_lon();
867 loc_lat = nav->get_lat();
868 nav_elev = nav->get_elev_ft();
869 twist = nav->get_multiuse();
870 range = nav->get_range();
871 effective_range = adjustNavRange(nav_elev, elev, range);
873 target_radial = sel_radial_node->getDoubleValue();
874 nav_xyz = nav->get_cart();
876 if ( globals->get_soundmgr()->exists( nav_fx_name ) ) {
877 globals->get_soundmgr()->remove( nav_fx_name );
880 SGSoundSample *sound;
881 sound = morse.make_ident( trans_ident, LO_FREQUENCY );
882 sound->set_volume( 0.3 );
883 if ( globals->get_soundmgr()->add( sound, nav_fx_name ) ) {
884 // cout << "Added nav-vor-ident sound" << endl;
886 SG_LOG(SG_COCKPIT, SG_WARN, "Failed to add v1-vor-ident sound");
889 if ( globals->get_soundmgr()->exists( dme_fx_name ) ) {
890 globals->get_soundmgr()->remove( dme_fx_name );
892 sound = morse.make_ident( trans_ident, HI_FREQUENCY );
893 sound->set_volume( 0.3 );
894 globals->get_soundmgr()->add( sound, dme_fx_name );
896 int offset = (int)(sg_random() * 30.0);
897 play_count = offset / 4;
898 last_time = globals->get_time_params()->get_cur_time() - offset;
899 // cout << "offset = " << offset << " play_count = "
900 // << play_count << " last_time = "
901 // << last_time << " current time = "
902 // << globals->get_time_params()->get_cur_time() << endl;
904 // cout << "Found a vor station in range" << endl;
905 // cout << " id = " << nav->get_ident() << endl;
906 } catch ( sg_io_exception &e ) {
907 SG_LOG(SG_GENERAL, SG_ALERT, e.getFormattedMessage());
912 nav_id_node->setStringValue( "" );
916 globals->get_soundmgr()->remove( nav_fx_name );
917 globals->get_soundmgr()->remove( dme_fx_name );
920 is_valid_node->setBoolValue( is_valid );
923 strncpy( tmpid, nav_id.c_str(), 5 );
924 id_c1_node->setIntValue( (int)tmpid[0] );
925 id_c2_node->setIntValue( (int)tmpid[1] );
926 id_c3_node->setIntValue( (int)tmpid[2] );
927 id_c4_node->setIntValue( (int)tmpid[3] );