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>
37 #include <Aircraft/aircraft.hxx>
38 #include <Navaids/navlist.hxx>
40 #include "navradio.hxx"
47 FGNavRadio::FGNavRadio(SGPropertyNode *node) :
48 lon_node(fgGetNode("/position/longitude-deg", true)),
49 lat_node(fgGetNode("/position/latitude-deg", true)),
50 alt_node(fgGetNode("/position/altitude-ft", true)),
55 sel_radial_node(NULL),
59 backcourse_node(NULL),
60 nav_serviceable_node(NULL),
61 cdi_serviceable_node(NULL),
62 gs_serviceable_node(NULL),
63 tofrom_serviceable_node(NULL),
65 fmt_alt_freq_node(NULL),
68 recip_radial_node(NULL),
69 target_radial_true_node(NULL),
70 target_auto_hdg_node(NULL),
71 time_to_intercept(NULL),
75 cdi_deflection_node(NULL),
76 cdi_xtrack_error_node(NULL),
77 cdi_xtrack_hdg_err_node(NULL),
81 gs_deflection_node(NULL),
82 gs_rate_of_climb_node(NULL),
89 nav_slaved_to_gps_node(NULL),
90 gps_cdi_deflection_node(NULL),
91 gps_to_flag_node(NULL),
92 gps_from_flag_node(NULL),
102 last_xtrack_error(0.0),
103 _name(node->getStringValue("name", "nav")),
104 _num(node->getIntValue("number", 0)),
105 _time_before_search_sec(-1.0)
107 SGPath path( globals->get_fg_root() );
109 term.append( "Navaids/range.term" );
111 low.append( "Navaids/range.low" );
113 high.append( "Navaids/range.high" );
115 term_tbl = new SGInterpTable( term.str() );
116 low_tbl = new SGInterpTable( low.str() );
117 high_tbl = new SGInterpTable( high.str() );
122 FGNavRadio::~FGNavRadio()
136 branch = "/instrumentation/" + _name;
138 SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
141 fgGetNode(("/systems/electrical/outputs/" + _name).c_str(), true);
144 is_valid_node = node->getChild("data-is-valid", 0, true);
145 power_btn_node = node->getChild("power-btn", 0, true);
146 power_btn_node->setBoolValue( true );
147 vol_btn_node = node->getChild("volume", 0, true);
148 ident_btn_node = node->getChild("ident", 0, true);
149 ident_btn_node->setBoolValue( true );
150 audio_btn_node = node->getChild("audio-btn", 0, true);
151 audio_btn_node->setBoolValue( true );
152 backcourse_node = node->getChild("back-course-btn", 0, true);
153 backcourse_node->setBoolValue( false );
154 nav_serviceable_node = node->getChild("serviceable", 0, true);
155 cdi_serviceable_node = (node->getChild("cdi", 0, true))
156 ->getChild("serviceable", 0, true);
157 gs_serviceable_node = (node->getChild("gs", 0, true))
158 ->getChild("serviceable");
159 tofrom_serviceable_node = (node->getChild("to-from", 0, true))
160 ->getChild("serviceable", 0, true);
163 SGPropertyNode *subnode = node->getChild("frequencies", 0, true);
164 freq_node = subnode->getChild("selected-mhz", 0, true);
165 alt_freq_node = subnode->getChild("standby-mhz", 0, true);
166 fmt_freq_node = subnode->getChild("selected-mhz-fmt", 0, true);
167 fmt_alt_freq_node = subnode->getChild("standby-mhz-fmt", 0, true);
170 subnode = node->getChild("radials", 0, true);
171 sel_radial_node = subnode->getChild("selected-deg", 0, true);
172 radial_node = subnode->getChild("actual-deg", 0, true);
173 recip_radial_node = subnode->getChild("reciprocal-radial-deg", 0, true);
174 target_radial_true_node = subnode->getChild("target-radial-deg", 0, true);
175 target_auto_hdg_node = subnode->getChild("target-auto-hdg-deg", 0, true);
178 heading_node = node->getChild("heading-deg", 0, true);
179 time_to_intercept = node->getChild("time-to-intercept-sec", 0, true);
180 to_flag_node = node->getChild("to-flag", 0, true);
181 from_flag_node = node->getChild("from-flag", 0, true);
182 inrange_node = node->getChild("in-range", 0, true);
183 cdi_deflection_node = node->getChild("heading-needle-deflection", 0, true);
184 cdi_xtrack_error_node = node->getChild("crosstrack-error-m", 0, true);
185 cdi_xtrack_hdg_err_node
186 = node->getChild("crosstrack-heading-error-deg", 0, true);
187 has_gs_node = node->getChild("has-gs", 0, true);
188 loc_node = node->getChild("nav-loc", 0, true);
189 loc_dist_node = node->getChild("nav-distance", 0, true);
190 gs_deflection_node = node->getChild("gs-needle-deflection", 0, true);
191 gs_rate_of_climb_node = node->getChild("gs-rate-of-climb", 0, true);
192 gs_dist_node = node->getChild("gs-distance", 0, true);
193 nav_id_node = node->getChild("nav-id", 0, true);
194 id_c1_node = node->getChild("nav-id_asc1", 0, true);
195 id_c2_node = node->getChild("nav-id_asc2", 0, true);
196 id_c3_node = node->getChild("nav-id_asc3", 0, true);
197 id_c4_node = node->getChild("nav-id_asc4", 0, true);
199 // gps slaving support
200 nav_slaved_to_gps_node = node->getChild("slaved-to-gps", 0, true);
201 gps_cdi_deflection_node = fgGetNode("/instrumentation/gps/cdi-deflection", true);
202 gps_to_flag_node = fgGetNode("/instrumentation/gps/to-flag", true);
203 gps_from_flag_node = fgGetNode("/instrumentation/gps/from-flag", true);
205 std::ostringstream temp;
206 temp << _name << "nav-ident" << _num;
207 nav_fx_name = temp.str();
208 temp << _name << "dme-ident" << _num;
209 dme_fx_name = temp.str();
215 std::ostringstream temp;
218 branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
223 FGNavRadio::unbind ()
225 std::ostringstream temp;
228 branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
232 // model standard VOR/DME/TACAN service volumes as per AIM 1-1-8
233 double FGNavRadio::adjustNavRange( double stationElev, double aircraftElev,
234 double nominalRange )
236 // extend out actual usable range to be 1.3x the published safe range
237 const double usability_factor = 1.3;
239 // assumptions we model the standard service volume, plus
240 // ... rather than specifying a cylinder, we model a cone that
241 // contains the cylinder. Then we put an upside down cone on top
242 // to model diminishing returns at too-high altitudes.
244 // altitude difference
245 double alt = ( aircraftElev * SG_METER_TO_FEET - stationElev );
246 // cout << "aircraft elev = " << aircraftElev * SG_METER_TO_FEET
247 // << " station elev = " << stationElev << endl;
249 if ( nominalRange < 25.0 + SG_EPSILON ) {
250 // Standard Terminal Service Volume
251 return term_tbl->interpolate( alt ) * usability_factor;
252 } else if ( nominalRange < 50.0 + SG_EPSILON ) {
253 // Standard Low Altitude Service Volume
254 // table is based on range of 40, scale to actual range
255 return low_tbl->interpolate( alt ) * nominalRange / 40.0
258 // Standard High Altitude Service Volume
259 // table is based on range of 130, scale to actual range
260 return high_tbl->interpolate( alt ) * nominalRange / 130.0
266 // model standard ILS service volumes as per AIM 1-1-9
267 double FGNavRadio::adjustILSRange( double stationElev, double aircraftElev,
268 double offsetDegrees, double distance )
270 // assumptions we model the standard service volume, plus
272 // altitude difference
273 // double alt = ( aircraftElev * SG_METER_TO_FEET - stationElev );
274 // double offset = fabs( offsetDegrees );
276 // if ( offset < 10 ) {
277 // return FG_ILS_DEFAULT_RANGE;
278 // } else if ( offset < 35 ) {
279 // return 10 + (35 - offset) * (FG_ILS_DEFAULT_RANGE - 10) / 25;
280 // } else if ( offset < 45 ) {
281 // return (45 - offset);
282 // } else if ( offset > 170 ) {
283 // return FG_ILS_DEFAULT_RANGE;
284 // } else if ( offset > 145 ) {
285 // return 10 + (offset - 145) * (FG_ILS_DEFAULT_RANGE - 10) / 25;
286 // } else if ( offset > 135 ) {
287 // return (offset - 135);
291 return FG_LOC_DEFAULT_RANGE;
295 //////////////////////////////////////////////////////////////////////////
296 // Update the various nav values based on position and valid tuned in navs
297 //////////////////////////////////////////////////////////////////////////
299 FGNavRadio::update(double dt)
301 // Do a nav station search only once a second to reduce
302 // unnecessary work. (Also, make sure to do this before caching
304 _time_before_search_sec -= dt;
305 if ( _time_before_search_sec < 0 ) {
309 // cache a few strategic values locally for speed
310 SGGeod pos = SGGeod::fromDegFt(lon_node->getDoubleValue(),
311 lat_node->getDoubleValue(),
312 alt_node->getDoubleValue());
313 bool power_btn = power_btn_node->getBoolValue();
314 bool nav_serviceable = nav_serviceable_node->getBoolValue();
315 bool cdi_serviceable = cdi_serviceable_node->getBoolValue();
316 bool tofrom_serviceable = tofrom_serviceable_node->getBoolValue();
317 bool inrange = inrange_node->getBoolValue();
318 bool has_gs = has_gs_node->getBoolValue();
319 bool is_loc = loc_node->getBoolValue();
320 double loc_dist = loc_dist_node->getDoubleValue();
324 // Create "formatted" versions of the nav frequencies for
325 // instrument displays.
327 sprintf( tmp, "%.2f", freq_node->getDoubleValue() );
328 fmt_freq_node->setStringValue(tmp);
329 sprintf( tmp, "%.2f", alt_freq_node->getDoubleValue() );
330 fmt_alt_freq_node->setStringValue(tmp);
332 // cout << "is_valid = " << is_valid
333 // << " power_btn = " << power_btn
334 // << " bus_power = " << bus_power_node->getDoubleValue()
335 // << " nav_serviceable = " << nav_serviceable
338 if ( is_valid && power_btn && (bus_power_node->getDoubleValue() > 1.0)
341 SGVec3d aircraft = SGVec3d::fromGeod(pos);
342 loc_dist = dist(aircraft, nav_xyz);
343 loc_dist_node->setDoubleValue( loc_dist );
344 // cout << "dt = " << dt << " dist = " << loc_dist << endl;
347 // find closest distance to the gs base line
348 SGVec3d p = aircraft;
349 double dist = sgdClosestPointToLineDistSquared(p.sg(), gs_xyz.sg(),
351 gs_dist_node->setDoubleValue( sqrt( dist ) );
352 // cout << "gs_dist = " << gs_dist_node->getDoubleValue()
355 // wgs84 heading to glide slope (to determine sign of distance)
356 geo_inverse_wgs_84( pos, SGGeod::fromDeg(gs_lon, gs_lat),
358 double r = az1 - target_radial;
359 while ( r > 180.0 ) { r -= 360.0;}
360 while ( r < -180.0 ) { r += 360.0;}
361 if ( r >= -90.0 && r <= 90.0 ) {
362 gs_dist_signed = gs_dist_node->getDoubleValue();
364 gs_dist_signed = -gs_dist_node->getDoubleValue();
366 /* cout << "Target Radial = " << target_radial
367 << " Bearing = " << az1
368 << " dist (signed) = " << gs_dist_signed
372 gs_dist_node->setDoubleValue( 0.0 );
375 //////////////////////////////////////////////////////////
376 // compute forward and reverse wgs84 headings to localizer
377 //////////////////////////////////////////////////////////
379 geo_inverse_wgs_84( pos, SGGeod::fromDeg(loc_lon, loc_lat),
381 // cout << "az1 = " << az1 << " magvar = " << nav_magvar << endl;
382 heading_node->setDoubleValue( hdg );
383 radial = az2 - twist;
384 double recip = radial + 180.0;
385 if ( recip >= 360.0 ) { recip -= 360.0; }
386 radial_node->setDoubleValue( radial );
387 recip_radial_node->setDoubleValue( recip );
388 // cout << " heading = " << heading_node->getDoubleValue()
389 // << " dist = " << nav_dist << endl;
391 //////////////////////////////////////////////////////////
392 // compute the target/selected radial in "true" heading
393 //////////////////////////////////////////////////////////
396 // ILS localizers radials are already "true" in our
398 trtrue = target_radial;
400 // VOR radials need to have that vor's offset added in
401 trtrue = target_radial + twist;
404 while ( trtrue < 0.0 ) { trtrue += 360.0; }
405 while ( trtrue > 360.0 ) { trtrue -= 360.0; }
406 target_radial_true_node->setDoubleValue( trtrue );
408 //////////////////////////////////////////////////////////
409 // adjust reception range for altitude
410 // FIXME: make sure we are using the navdata range now that
411 // it is valid in the data file
412 //////////////////////////////////////////////////////////
414 double offset = radial - target_radial;
415 while ( offset < -180.0 ) { offset += 360.0; }
416 while ( offset > 180.0 ) { offset -= 360.0; }
417 // cout << "ils offset = " << offset << endl;
419 = adjustILSRange( nav_elev, pos.getElevationM(), offset,
420 loc_dist * SG_METER_TO_NM );
423 = adjustNavRange( nav_elev, pos.getElevationM(), range );
425 // cout << "nav range = " << effective_range
426 // << " (" << range << ")" << endl;
428 if ( loc_dist < effective_range * SG_NM_TO_METER ) {
430 } else if ( loc_dist < 2 * effective_range * SG_NM_TO_METER ) {
431 inrange = sg_random() < ( 2 * effective_range * SG_NM_TO_METER
433 / (effective_range * SG_NM_TO_METER);
437 inrange_node->setBoolValue( inrange );
440 target_radial = sel_radial_node->getDoubleValue();
443 //////////////////////////////////////////////////////////
444 // compute to/from flag status
445 //////////////////////////////////////////////////////////
447 double offset = fabs(radial - target_radial);
448 if ( tofrom_serviceable ) {
449 if ( nav_slaved_to_gps_node->getBoolValue() ) {
450 value = gps_to_flag_node->getBoolValue();
451 } else if ( inrange ) {
455 value = !(offset <= 90.0 || offset >= 270.0);
461 to_flag_node->setBoolValue( value );
464 if ( tofrom_serviceable ) {
465 if ( nav_slaved_to_gps_node->getBoolValue() ) {
466 value = gps_from_flag_node->getBoolValue();
467 } else if ( inrange ) {
471 value = !(offset > 90.0 && offset < 270.0);
477 from_flag_node->setBoolValue( value );
479 //////////////////////////////////////////////////////////
480 // compute the deflection of the CDI needle, clamped to the range
482 //////////////////////////////////////////////////////////
484 bool loc_backside = false; // an in-code flag indicating that we are
485 // on a localizer backcourse.
486 if ( cdi_serviceable ) {
487 if ( nav_slaved_to_gps_node->getBoolValue() ) {
488 r = gps_cdi_deflection_node->getDoubleValue();
489 // We want +- 5 dots deflection for the gps, so clamp
491 SG_CLAMP_RANGE( r, -12.5, 12.5 );
492 } else if ( inrange ) {
493 r = radial - target_radial;
494 // cout << "Target radial = " << target_radial
495 // << " Actual radial = " << radial << endl;
497 while ( r > 180.0 ) { r -= 360.0;}
498 while ( r < -180.0 ) { r += 360.0;}
499 if ( fabs(r) > 90.0 ) {
500 r = ( r<0.0 ? -r-180.0 : -r+180.0 );
507 r = -r; // reverse, since radial is outbound
509 // According to Robin Peel, the ILS is 4x more
510 // sensitive than a vor
513 SG_CLAMP_RANGE( r, -10.0, 10.0 );
516 cdi_deflection_node->setDoubleValue( r );
518 //////////////////////////////////////////////////////////
519 // compute the amount of cross track distance error in meters
520 //////////////////////////////////////////////////////////
521 double xtrack_error = 0.0;
522 if ( inrange && nav_serviceable && cdi_serviceable ) {
523 r = radial - target_radial;
524 // cout << "Target radial = " << target_radial
525 // << " Actual radial = " << radial
526 // << " r = " << r << endl;
528 while ( r > 180.0 ) { r -= 360.0;}
529 while ( r < -180.0 ) { r += 360.0;}
530 if ( fabs(r) > 90.0 ) {
531 r = ( r<0.0 ? -r-180.0 : -r+180.0 );
534 r = -r; // reverse, since radial is outbound
536 xtrack_error = loc_dist * sin(r * SGD_DEGREES_TO_RADIANS);
540 cdi_xtrack_error_node->setDoubleValue( xtrack_error );
542 //////////////////////////////////////////////////////////
543 // compute an approximate ground track heading error
544 //////////////////////////////////////////////////////////
545 double hdg_error = 0.0;
546 if ( inrange && cdi_serviceable ) {
547 double vn = fgGetDouble( "/velocities/speed-north-fps" );
548 double ve = fgGetDouble( "/velocities/speed-east-fps" );
549 double gnd_trk_true = atan2( ve, vn ) * SGD_RADIANS_TO_DEGREES;
550 if ( gnd_trk_true < 0.0 ) { gnd_trk_true += 360.0; }
552 SGPropertyNode *true_hdg
553 = fgGetNode("/orientation/heading-deg", true);
554 hdg_error = gnd_trk_true - true_hdg->getDoubleValue();
556 // cout << "ground track = " << gnd_trk_true
557 // << " orientation = " << true_hdg->getDoubleValue() << endl;
559 cdi_xtrack_hdg_err_node->setDoubleValue( hdg_error );
561 //////////////////////////////////////////////////////////
562 // compute the time to intercept selected radial (based on
563 // current and last cross track errors and dt
564 //////////////////////////////////////////////////////////
566 if ( inrange && cdi_serviceable ) {
567 double xrate_ms = (last_xtrack_error - xtrack_error) / dt;
568 if ( fabs(xrate_ms) > 0.00001 ) {
569 t = xtrack_error / xrate_ms;
574 time_to_intercept->setDoubleValue( t );
576 //////////////////////////////////////////////////////////
577 // compute the amount of glide slope needle deflection
578 // (.i.e. the number of degrees we are off the glide slope * 5.0
580 // CLO - 13 Mar 2006: The glide slope needle should peg at
581 // +/-0.7 degrees off the ideal glideslope. I'm not sure why
582 // we compute the factor the way we do (5*gs_error), but we
583 // need to compensate for our 'odd' number in the glideslope
584 // needle animation. This means that the needle should peg
585 // when this values is +/-3.5.
586 //////////////////////////////////////////////////////////
588 if ( has_gs && gs_serviceable_node->getBoolValue() ) {
589 if ( nav_slaved_to_gps_node->getBoolValue() ) {
590 // FIXME/FINISHME, what should be set here?
591 } else if ( inrange ) {
592 double x = gs_dist_node->getDoubleValue();
593 double y = (fgGetDouble("/position/altitude-ft") - nav_elev)
595 // cout << "dist = " << x << " height = " << y << endl;
596 double angle = asin( y / x ) * SGD_RADIANS_TO_DEGREES;
597 r = (target_gs - angle) * 5.0;
600 gs_deflection_node->setDoubleValue( r );
602 //////////////////////////////////////////////////////////
603 // Calculate desired rate of climb for intercepting the GS
604 //////////////////////////////////////////////////////////
605 double x = gs_dist_node->getDoubleValue();
606 double y = (alt_node->getDoubleValue() - nav_elev)
608 double current_angle = atan2( y, x ) * SGD_RADIANS_TO_DEGREES;
610 double target_angle = target_gs;
611 double gs_diff = target_angle - current_angle;
613 // convert desired vertical path angle into a climb rate
614 double des_angle = current_angle - 10 * gs_diff;
616 // estimate horizontal speed towards ILS in meters per minute
617 double dist = last_x - x;
621 double new_vel = ( dist / dt );
623 horiz_vel = 0.75 * horiz_vel + 0.25 * new_vel;
624 // double horiz_vel = cur_fdm_state->get_V_ground_speed()
625 // * SG_FEET_TO_METER * 60.0;
626 // double horiz_vel = airspeed_node->getFloatValue()
627 // * SG_FEET_TO_METER * 60.0;
629 gs_rate_of_climb_node
630 ->setDoubleValue( -sin( des_angle * SGD_DEGREES_TO_RADIANS )
631 * horiz_vel * SG_METER_TO_FEET );
634 //////////////////////////////////////////////////////////
635 // Calculate a suggested target heading to smoothly intercept
637 //////////////////////////////////////////////////////////
639 // Now that we have cross track heading adjustment built in,
640 // we shouldn't need to overdrive the heading angle within 8km
643 // The cdi deflection should be +/-10 for a full range of deflection
644 // so multiplying this by 3 gives us +/- 30 degrees heading
646 double adjustment = cdi_deflection_node->getDoubleValue() * 3.0;
647 SG_CLAMP_RANGE( adjustment, -30.0, 30.0 );
649 // determine the target heading to fly to intercept the
650 // tgt_radial = target radial (true) + cdi offset adjustmest -
651 // xtrack heading error adjustment
653 if ( is_loc && backcourse_node->getBoolValue() ) {
654 // tuned to a localizer and backcourse mode activated
655 trtrue += 180.0; // reverse the target localizer heading
656 while ( trtrue > 360.0 ) { trtrue -= 360.0; }
657 nta_hdg = trtrue - adjustment - hdg_error;
659 nta_hdg = trtrue + adjustment - hdg_error;
662 while ( nta_hdg < 0.0 ) { nta_hdg += 360.0; }
663 while ( nta_hdg >= 360.0 ) { nta_hdg -= 360.0; }
664 target_auto_hdg_node->setDoubleValue( nta_hdg );
666 last_xtrack_error = xtrack_error;
668 inrange_node->setBoolValue( false );
669 cdi_deflection_node->setDoubleValue( 0.0 );
670 cdi_xtrack_error_node->setDoubleValue( 0.0 );
671 cdi_xtrack_hdg_err_node->setDoubleValue( 0.0 );
672 time_to_intercept->setDoubleValue( 0.0 );
673 gs_deflection_node->setDoubleValue( 0.0 );
674 to_flag_node->setBoolValue( false );
675 from_flag_node->setBoolValue( false );
676 // cout << "not picking up vor. :-(" << endl;
680 if ( is_valid && inrange && nav_serviceable ) {
681 // play station ident via audio system if on + ident,
682 // otherwise turn it off
684 && (bus_power_node->getDoubleValue() > 1.0)
685 && ident_btn_node->getBoolValue()
686 && audio_btn_node->getBoolValue() )
688 SGSoundSample *sound;
689 sound = globals->get_soundmgr()->find( nav_fx_name );
690 double vol = vol_btn_node->getDoubleValue();
691 if ( vol < 0.0 ) { vol = 0.0; }
692 if ( vol > 1.0 ) { vol = 1.0; }
693 if ( sound != NULL ) {
694 sound->set_volume( vol );
696 SG_LOG( SG_COCKPIT, SG_ALERT,
697 "Can't find nav-vor-ident sound" );
699 sound = globals->get_soundmgr()->find( dme_fx_name );
700 if ( sound != NULL ) {
701 sound->set_volume( vol );
703 SG_LOG( SG_COCKPIT, SG_ALERT,
704 "Can't find nav-dme-ident sound" );
706 // cout << "last_time = " << last_time << " ";
707 // cout << "cur_time = "
708 // << globals->get_time_params()->get_cur_time();
710 globals->get_time_params()->get_cur_time() - 30 ) {
711 last_time = globals->get_time_params()->get_cur_time();
714 // cout << " play_count = " << play_count << endl;
715 // cout << "playing = "
716 // << globals->get_soundmgr()->is_playing(nav_fx_name)
718 if ( play_count < 4 ) {
720 if ( !globals->get_soundmgr()->is_playing(nav_fx_name) ) {
721 globals->get_soundmgr()->play_once( nav_fx_name );
724 } else if ( play_count < 5 && has_dme ) {
726 if ( !globals->get_soundmgr()->is_playing(nav_fx_name) &&
727 !globals->get_soundmgr()->is_playing(dme_fx_name) ) {
728 globals->get_soundmgr()->play_once( dme_fx_name );
733 globals->get_soundmgr()->stop( nav_fx_name );
734 globals->get_soundmgr()->stop( dme_fx_name );
738 last_loc_dist = loc_dist;
742 // Update current nav/adf radio stations based on current postition
743 void FGNavRadio::search()
747 _time_before_search_sec = 1.0;
749 // cache values locally for speed
750 double lon = lon_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
751 double lat = lat_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
752 double elev = alt_node->getDoubleValue() * SG_FEET_TO_METER;
754 FGNavRecord *nav = NULL;
755 FGNavRecord *loc = NULL;
756 FGNavRecord *dme = NULL;
757 FGNavRecord *gs = NULL;
759 ////////////////////////////////////////////////////////////////////////
761 ////////////////////////////////////////////////////////////////////////
763 double freq = freq_node->getDoubleValue();
764 nav = globals->get_navlist()->findByFreq(freq, lon, lat, elev);
765 dme = globals->get_dmelist()->findByFreq(freq, lon, lat, elev);
767 loc = globals->get_loclist()->findByFreq(freq, lon, lat, elev);
768 gs = globals->get_gslist()->findByFreq(freq, lon, lat, elev);
774 nav_id = loc->get_ident();
775 nav_id_node->setStringValue( nav_id.c_str() );
776 // cout << "localizer = " << nav_id_node->getStringValue() << endl;
778 if ( last_nav_id != nav_id || last_nav_vor ) {
779 trans_ident = loc->get_trans_ident();
780 target_radial = loc->get_multiuse();
781 while ( target_radial < 0.0 ) { target_radial += 360.0; }
782 while ( target_radial > 360.0 ) { target_radial -= 360.0; }
783 loc_lon = loc->get_lon();
784 loc_lat = loc->get_lat();
785 nav_xyz = loc->get_cart();
786 last_nav_id = nav_id;
787 last_nav_vor = false;
788 loc_node->setBoolValue( true );
789 has_dme = (dme != NULL);
791 has_gs_node->setBoolValue( true );
792 gs_lon = gs->get_lon();
793 gs_lat = gs->get_lat();
794 nav_elev = gs->get_elev_ft();
795 int tmp = (int)(gs->get_multiuse() / 1000.0);
796 target_gs = (double)tmp / 100.0;
797 gs_xyz = gs->get_cart();
799 // derive GS baseline (perpendicular to the runay
801 double tlon, tlat, taz;
802 geo_direct_wgs_84 ( 0.0, gs_lat, gs_lon,
804 100.0, &tlat, &tlon, &taz );
805 // cout << "target_radial = " << target_radial << endl;
806 // cout << "nav_loc = " << loc_node->getBoolValue() << endl;
807 // cout << gs_lon << "," << gs_lat << " "
808 // << tlon << "," << tlat << " (" << nav_elev << ")"
810 SGGeod tpos = SGGeod::fromDegFt(tlon, tlat, nav_elev);
811 SGVec3d p1 = SGVec3d::fromGeod(tpos);
813 // cout << gs_xyz << endl;
814 // cout << p1 << endl;
815 gs_base_vec = p1 - gs_xyz;
816 // cout << gs_base_vec << endl;
818 has_gs_node->setBoolValue( false );
819 nav_elev = loc->get_elev_ft();
822 range = FG_LOC_DEFAULT_RANGE;
823 effective_range = range;
825 if ( globals->get_soundmgr()->exists( nav_fx_name ) ) {
826 globals->get_soundmgr()->remove( nav_fx_name );
828 SGSoundSample *sound;
829 sound = morse.make_ident( trans_ident, LO_FREQUENCY );
830 sound->set_volume( 0.3 );
831 globals->get_soundmgr()->add( sound, nav_fx_name );
833 if ( globals->get_soundmgr()->exists( dme_fx_name ) ) {
834 globals->get_soundmgr()->remove( dme_fx_name );
836 sound = morse.make_ident( trans_ident, HI_FREQUENCY );
837 sound->set_volume( 0.3 );
838 globals->get_soundmgr()->add( sound, dme_fx_name );
840 int offset = (int)(sg_random() * 30.0);
841 play_count = offset / 4;
842 last_time = globals->get_time_params()->get_cur_time() -
844 // cout << "offset = " << offset << " play_count = "
846 // << " last_time = " << last_time
847 // << " current time = "
848 // << globals->get_time_params()->get_cur_time() << endl;
850 // cout << "Found an loc station in range" << endl;
851 // cout << " id = " << loc->get_locident() << endl;
853 } else if ( nav != NULL ) {
854 nav_id = nav->get_ident();
855 nav_id_node->setStringValue( nav_id.c_str() );
856 // cout << "nav = " << nav_id << endl;
858 if ( last_nav_id != nav_id || !last_nav_vor ) {
859 last_nav_id = nav_id;
861 trans_ident = nav->get_trans_ident();
862 loc_node->setBoolValue( false );
863 has_dme = (dme != NULL);
864 has_gs_node->setBoolValue( false );
865 loc_lon = nav->get_lon();
866 loc_lat = nav->get_lat();
867 nav_elev = nav->get_elev_ft();
868 twist = nav->get_multiuse();
869 range = nav->get_range();
870 effective_range = adjustNavRange(nav_elev, elev, range);
872 target_radial = sel_radial_node->getDoubleValue();
873 nav_xyz = nav->get_cart();
875 if ( globals->get_soundmgr()->exists( nav_fx_name ) ) {
876 globals->get_soundmgr()->remove( nav_fx_name );
879 SGSoundSample *sound;
880 sound = morse.make_ident( trans_ident, LO_FREQUENCY );
881 sound->set_volume( 0.3 );
882 if ( globals->get_soundmgr()->add( sound, nav_fx_name ) ) {
883 // cout << "Added nav-vor-ident sound" << endl;
885 SG_LOG(SG_COCKPIT, SG_WARN, "Failed to add v1-vor-ident sound");
888 if ( globals->get_soundmgr()->exists( dme_fx_name ) ) {
889 globals->get_soundmgr()->remove( dme_fx_name );
891 sound = morse.make_ident( trans_ident, HI_FREQUENCY );
892 sound->set_volume( 0.3 );
893 globals->get_soundmgr()->add( sound, dme_fx_name );
895 int offset = (int)(sg_random() * 30.0);
896 play_count = offset / 4;
897 last_time = globals->get_time_params()->get_cur_time() - offset;
898 // cout << "offset = " << offset << " play_count = "
899 // << play_count << " last_time = "
900 // << last_time << " current time = "
901 // << globals->get_time_params()->get_cur_time() << endl;
903 // cout << "Found a vor station in range" << endl;
904 // cout << " id = " << nav->get_ident() << endl;
905 } catch ( sg_io_exception &e ) {
906 SG_LOG(SG_GENERAL, SG_ALERT, e.getFormattedMessage());
911 nav_id_node->setStringValue( "" );
915 globals->get_soundmgr()->remove( nav_fx_name );
916 globals->get_soundmgr()->remove( dme_fx_name );
919 is_valid_node->setBoolValue( is_valid );
922 strncpy( tmpid, nav_id.c_str(), 5 );
923 id_c1_node->setIntValue( (int)tmpid[0] );
924 id_c2_node->setIntValue( (int)tmpid[1] );
925 id_c3_node->setIntValue( (int)tmpid[2] );
926 id_c4_node->setIntValue( (int)tmpid[3] );