1 // radio.cxx -- implementation of FGRadio
2 // Class to manage radio propagation using the ITM model
3 // Written by Adrian Musceac, started August 2011.
5 // This program is free software; you can redistribute it and/or
6 // modify it under the terms of the GNU General Public License as
7 // published by the Free Software Foundation; either version 2 of the
8 // License, or (at your option) any later version.
10 // This program is distributed in the hope that it will be useful, but
11 // WITHOUT ANY WARRANTY; without even the implied warranty of
12 // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
13 // General Public License for more details.
15 // You should have received a copy of the GNU General Public License
16 // along with this program; if not, write to the Free Software
17 // Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
29 #include <Scenery/scenery.hxx>
31 #define WITH_POINT_TO_POINT 1
37 /** radio parameters (which should probably be set for each radio) */
39 _receiver_sensitivity = -110.0; // typical AM receiver sensitivity seems to be 0.8 microVolt at 12dB SINAD
41 /** AM transmitter power in dBm.
42 * Note this value is calculated from the typical final transistor stage output
43 * small aircraft have portable transmitters which operate at 36 dBm output (4 Watts)
44 * later possibly store this value in aircraft description
45 * ATC comms usually operate high power equipment, thus making the link asymetrical; this is taken care of in propagation routines
47 _transmitter_power = 43.0;
49 /** pilot plane's antenna gain + AI aircraft antenna gain
50 * real-life gain for conventional monopole/dipole antenna
53 _propagation_model = 2; // choose between models via option: realistic radio on/off
62 double FGRadio::getFrequency(int radio) {
66 freq = fgGetDouble("/instrumentation/comm[0]/frequencies/selected-mhz");
69 freq = fgGetDouble("/instrumentation/comm[1]/frequencies/selected-mhz");
72 freq = fgGetDouble("/instrumentation/comm[0]/frequencies/selected-mhz");
78 /*** TODO: receive multiplayer chat message and voice
80 void FGRadio::receiveChat(SGGeod tx_pos, double freq, string text,
85 /*** Receive ATC radio communication as text
87 void FGRadio::receiveATC(SGGeod tx_pos, double freq, string text,
91 double comm1 = getFrequency(1);
92 double comm2 = getFrequency(2);
93 if ( (freq != comm1) && (freq != comm2) ) {
94 cerr << "Frequency not tuned: " << freq << " Radio1: " << comm1 << " Radio2: " << comm2 << endl;
99 if ( _propagation_model == 0) {
100 fgSetString("/sim/messages/atc", text.c_str());
102 else if ( _propagation_model == 1 ) {
103 // TODO: free space, round earth
104 double signal = LOS_calculate_attenuation(tx_pos, freq, ground_to_air);
106 SG_LOG(SG_GENERAL, SG_BULK, "Signal below receiver minimum sensitivity: " << signal);
107 //cerr << "Signal below receiver minimum sensitivity: " << signal << endl;
111 SG_LOG(SG_GENERAL, SG_BULK, "Signal completely readable: " << signal);
112 //cerr << "Signal completely readable: " << signal << endl;
113 fgSetString("/sim/messages/atc", text.c_str());
114 fgSetDouble("/sim/radio/comm1-signal", signal);
117 else if ( _propagation_model == 2 ) {
118 // Use ITM propagation model
119 double signal = ITM_calculate_attenuation(tx_pos, freq, ground_to_air);
121 SG_LOG(SG_GENERAL, SG_BULK, "Signal below receiver minimum sensitivity: " << signal);
122 //cerr << "Signal below receiver minimum sensitivity: " << signal << endl;
125 if ((signal > 0.0) && (signal < 12.0)) {
126 /** for low SNR values implement a way to make the conversation
127 * hard to understand but audible
128 * in the real world, the receiver AGC fails to capture the slope
129 * and the signal, due to being amplitude modulated, decreases volume after demodulation
130 * the workaround below is more akin to what would happen on a FM transmission
131 * therefore the correct way would be to work on the volume
134 string hash_noise = " ";
135 int reps = (int) (fabs(floor(signal - 11.0)) * 2);
136 int t_size = text.size();
137 for (int n = 1; n <= reps; ++n) {
138 int pos = rand() % (t_size -1);
139 text.replace(pos,1, hash_noise);
142 double volume = (fabs(signal - 12.0) / 12);
143 double old_volume = fgGetDouble("/sim/sound/voices/voice/volume");
144 SG_LOG(SG_GENERAL, SG_BULK, "Usable signal at limit: " << signal);
145 //cerr << "Usable signal at limit: " << signal << endl;
146 fgSetDouble("/sim/sound/voices/voice/volume", volume);
147 fgSetString("/sim/messages/atc", text.c_str());
148 fgSetDouble("/sim/radio/comm1-signal", signal);
149 fgSetDouble("/sim/sound/voices/voice/volume", old_volume);
152 SG_LOG(SG_GENERAL, SG_BULK, "Signal completely readable: " << signal);
153 //cerr << "Signal completely readable: " << signal << endl;
154 fgSetString("/sim/messages/atc", text.c_str());
155 fgSetDouble("/sim/radio/comm1-signal", signal);
164 /*** Implement radio attenuation
165 based on the Longley-Rice propagation model
167 double FGRadio::ITM_calculate_attenuation(SGGeod pos, double freq,
168 int transmission_type) {
172 /** ITM default parameters
173 TODO: take them from tile materials (especially for sea)?
175 double eps_dielect=15.0;
176 double sgm_conductivity = 0.005;
179 if( (freq < 118.0) || (freq > 137.0) )
180 frq_mhz = 125.0; // sane value, middle of bandplan
183 int radio_climate = 5; // continental temperate
184 int pol=1; // assuming vertical polarization although this is more complex in reality
185 double conf = 0.90; // 90% of situations and time, take into account speed
191 double tx_pow = _transmitter_power;
192 double ant_gain = _antenna_gain;
195 if(transmission_type == 1)
196 tx_pow = _transmitter_power + 6.0;
198 if((transmission_type == 1) || (transmission_type == 3))
199 ant_gain = _antenna_gain + 3.0; //pilot plane's antenna gain + ground station antenna gain
201 double link_budget = tx_pow - _receiver_sensitivity + ant_gain;
203 FGScenery * scenery = globals->get_scenery();
205 double own_lat = fgGetDouble("/position/latitude-deg");
206 double own_lon = fgGetDouble("/position/longitude-deg");
207 double own_alt_ft = fgGetDouble("/position/altitude-ft");
208 double own_alt= own_alt_ft * SG_FEET_TO_METER;
211 //cerr << "ITM:: pilot Lat: " << own_lat << ", Lon: " << own_lon << ", Alt: " << own_alt << endl;
213 SGGeod own_pos = SGGeod::fromDegM( own_lon, own_lat, own_alt );
214 SGGeod max_own_pos = SGGeod::fromDegM( own_lon, own_lat, SG_MAX_ELEVATION_M );
215 SGGeoc center = SGGeoc::fromGeod( max_own_pos );
216 SGGeoc own_pos_c = SGGeoc::fromGeod( own_pos );
218 /** position of sender radio antenna (HAAT)
219 sender can be aircraft or ground station
221 double ATC_HAAT = 30.0;
222 double Aircraft_HAAT = 5.0;
223 double sender_alt_ft,sender_alt;
224 double transmitter_height=0.0;
225 double receiver_height=0.0;
226 SGGeod sender_pos = pos;
228 sender_alt_ft = sender_pos.getElevationFt();
229 sender_alt = sender_alt_ft * SG_FEET_TO_METER;
230 SGGeod max_sender_pos = SGGeod::fromGeodM( pos, SG_MAX_ELEVATION_M );
231 SGGeoc sender_pos_c = SGGeoc::fromGeod( sender_pos );
232 //cerr << "ITM:: sender Lat: " << parent->getLatitude() << ", Lon: " << parent->getLongitude() << ", Alt: " << sender_alt << endl;
234 double point_distance= 90.0; // regular SRTM is 90 meters
235 double course = SGGeodesy::courseRad(own_pos_c, sender_pos_c);
236 double distance_m = SGGeodesy::distanceM(own_pos, sender_pos);
237 double probe_distance = 0.0;
238 /** If distance larger than this value (300 km), assume reception imposssible */
239 if (distance_m > 300000)
241 /** If above 8000 meters, consider LOS mode and calculate free-space att */
242 if (own_alt > 8000) {
243 dbloss = 20 * log10(distance_m) +20 * log10(frq_mhz) -27.55;
244 SG_LOG(SG_GENERAL, SG_BULK,
245 "ITM Free-space mode:: Link budget: " << link_budget << ", Attenuation: " << dbloss << " dBm, free-space attenuation");
246 //cerr << "ITM Free-space mode:: Link budget: " << link_budget << ", Attenuation: " << dbloss << " dBm, free-space attenuation" << endl;
247 signal = link_budget - dbloss;
252 double max_points = distance_m / point_distance;
253 deque<double> _elevations;
255 double elevation_under_pilot = 0.0;
256 if (scenery->get_elevation_m( max_own_pos, elevation_under_pilot, NULL )) {
257 receiver_height = own_alt - elevation_under_pilot + 3; //assume antenna located 3 meters above ground
260 double elevation_under_sender = 0.0;
261 if (scenery->get_elevation_m( max_sender_pos, elevation_under_sender, NULL )) {
262 transmitter_height = sender_alt - elevation_under_sender;
265 transmitter_height = sender_alt;
268 if(transmission_type == 1)
269 transmitter_height += ATC_HAAT;
271 transmitter_height += Aircraft_HAAT;
273 SG_LOG(SG_GENERAL, SG_BULK,
274 "ITM:: RX-height: " << receiver_height << " meters, TX-height: " << transmitter_height << " meters, Distance: " << distance_m << " meters");
275 cerr << "ITM:: RX-height: " << receiver_height << " meters, TX-height: " << transmitter_height << " meters, Distance: " << distance_m << " meters" << endl;
277 unsigned int e_size = (deque<unsigned>::size_type)max_points;
279 while (_elevations.size() <= e_size) {
280 probe_distance += point_distance;
281 SGGeod probe = SGGeod::fromGeoc(center.advanceRadM( course, probe_distance ));
283 double elevation_m = 0.0;
285 if (scenery->get_elevation_m( probe, elevation_m, NULL )) {
286 if((transmission_type == 3) || (transmission_type == 4)) {
287 _elevations.push_back(elevation_m);
290 _elevations.push_front(elevation_m);
294 if((transmission_type == 3) || (transmission_type == 4)) {
295 _elevations.push_back(elevation_m);
298 _elevations.push_front(0.0);
302 if((transmission_type == 3) || (transmission_type == 4)) {
303 _elevations.push_front(elevation_under_pilot);
304 _elevations.push_back(elevation_under_sender);
307 _elevations.push_back(elevation_under_pilot);
308 _elevations.push_front(elevation_under_sender);
312 double max_alt_between=0.0;
313 for( deque<double>::size_type i = 0; i < _elevations.size(); i++ ) {
314 if (_elevations[i] > max_alt_between) {
315 max_alt_between = _elevations[i];
319 double num_points= (double)_elevations.size();
320 //cerr << "ITM:: Max alt between: " << max_alt_between << ", num points:" << num_points << endl;
321 _elevations.push_front(point_distance);
322 _elevations.push_front(num_points -1);
323 int size = _elevations.size();
324 double itm_elev[size];
325 for(int i=0;i<size;i++) {
326 itm_elev[i]=_elevations[i];
327 //cerr << "ITM:: itm_elev: " << _elevations[i] << endl;
331 /** first Fresnel zone radius
332 frequency in the middle of the bandplan, more accuracy is not necessary
334 double fz_clr= 8.657 * sqrt(distance_m / 0.125);
336 // TODO: If we clear the first Fresnel zone, we are into line of sight territory
338 // else we need to calculate point to point link loss
339 if((transmission_type == 3) || (transmission_type == 4)) {
340 // the sender and receiver roles are switched
341 point_to_point(itm_elev, receiver_height, transmitter_height,
342 eps_dielect, sgm_conductivity, eno, frq_mhz, radio_climate,
343 pol, conf, rel, dbloss, strmode, errnum);
348 point_to_point(itm_elev, transmitter_height, receiver_height,
349 eps_dielect, sgm_conductivity, eno, frq_mhz, radio_climate,
350 pol, conf, rel, dbloss, strmode, errnum);
352 SG_LOG(SG_GENERAL, SG_BULK,
353 "ITM:: Link budget: " << link_budget << ", Attenuation: " << dbloss << " dBm, " << strmode << ", Error: " << errnum);
354 cerr << "ITM:: Link budget: " << link_budget << ", Attenuation: " << dbloss << " dBm, " << strmode << ", Error: " << errnum << endl;
356 //if (errnum == 4) // if parameters are outside sane values for lrprop, the alternative method is used
358 signal = link_budget - dbloss;
363 /*** implement simple LOS propagation model (WIP)
365 double FGRadio::LOS_calculate_attenuation(SGGeod pos, double freq,
366 int transmission_type) {
368 if( (freq < 118.0) || (freq > 137.0) )
369 frq_mhz = 125.0; // sane value, middle of bandplan
373 double tx_pow = _transmitter_power;
374 double ant_gain = _antenna_gain;
376 double ATC_HAAT = 30.0;
377 double Aircraft_HAAT = 5.0;
378 double sender_alt_ft,sender_alt;
379 double transmitter_height=0.0;
380 double receiver_height=0.0;
381 double own_lat = fgGetDouble("/position/latitude-deg");
382 double own_lon = fgGetDouble("/position/longitude-deg");
383 double own_alt_ft = fgGetDouble("/position/altitude-ft");
384 double own_alt= own_alt_ft * SG_FEET_TO_METER;
386 if(transmission_type == 1)
387 tx_pow = _transmitter_power + 6.0;
389 if((transmission_type == 1) || (transmission_type == 3))
390 ant_gain = _antenna_gain + 3.0; //pilot plane's antenna gain + ground station antenna gain
392 double link_budget = tx_pow - _receiver_sensitivity + ant_gain;
394 //cerr << "ITM:: pilot Lat: " << own_lat << ", Lon: " << own_lon << ", Alt: " << own_alt << endl;
396 SGGeod own_pos = SGGeod::fromDegM( own_lon, own_lat, own_alt );
398 SGGeod sender_pos = pos;
400 sender_alt_ft = sender_pos.getElevationFt();
401 sender_alt = sender_alt_ft * SG_FEET_TO_METER;
403 receiver_height = own_alt;
404 transmitter_height = sender_alt;
406 double distance_m = SGGeodesy::distanceM(own_pos, sender_pos);
408 if(transmission_type == 1)
409 transmitter_height += ATC_HAAT;
411 transmitter_height += Aircraft_HAAT;
413 /** radio horizon calculation with wave bending k=4/3 */
414 double receiver_horizon = 4.12 * sqrt(receiver_height);
415 double transmitter_horizon = 4.12 * sqrt(transmitter_height);
416 double total_horizon = receiver_horizon + transmitter_horizon;
418 if (distance_m > total_horizon) {
422 // free-space loss (distance calculation should be changed)
423 dbloss = 20 * log10(distance_m) +20 * log10(frq_mhz) -27.55;
424 signal = link_budget - dbloss;
425 SG_LOG(SG_GENERAL, SG_BULK,
426 "LOS:: Link budget: " << link_budget << ", Attenuation: " << dbloss << " dBm ");
427 cerr << "LOS:: Link budget: " << link_budget << ", Attenuation: " << dbloss << " dBm " << endl;