988de9dbca
by frequency (which makes sense), and use the FGPositioned spatial data if required. As a result, the marker beacon list is gone (since beacons are only searched spatially). In the process, clean up various minor things - most notably, all the 'airport-related' navaids (ILS, GS, LOC, and the beacons) now store a FGRunway* instead of an airport id string. This is more precise, and saves string allocations.
182 lines
5.7 KiB
C++
182 lines
5.7 KiB
C++
// dme.cxx - distance-measuring equipment.
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// Written by David Megginson, started 2003.
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//
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// This file is in the Public Domain and comes with no warranty.
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#ifdef HAVE_CONFIG_H
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# include <config.h>
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#endif
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#include <simgear/compiler.h>
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#include <simgear/math/sg_geodesy.hxx>
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#include <simgear/math/sg_random.h>
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#include <Main/fg_props.hxx>
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#include <Navaids/navlist.hxx>
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#include "dme.hxx"
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/**
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* Adjust the range.
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*
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* Start by calculating the radar horizon based on the elevation
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* difference, then clamp to the maximum, then add a fudge for
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* borderline reception.
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*/
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static double
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adjust_range (double transmitter_elevation_ft, double aircraft_altitude_ft,
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double max_range_nm)
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{
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double delta_elevation_ft =
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fabs(aircraft_altitude_ft - transmitter_elevation_ft);
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double range_nm = 1.23 * sqrt(delta_elevation_ft);
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if (range_nm > max_range_nm)
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range_nm = max_range_nm;
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else if (range_nm < 20.0)
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range_nm = 20.0;
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double rand = sg_random();
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return range_nm + (range_nm * rand * rand);
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}
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DME::DME ( SGPropertyNode *node )
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: _last_distance_nm(0),
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_last_frequency_mhz(-1),
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_time_before_search_sec(0),
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_transmitter_valid(false),
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_transmitter_elevation_ft(0),
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_transmitter_range_nm(0),
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_transmitter_bias(0.0),
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_name(node->getStringValue("name", "dme")),
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_num(node->getIntValue("number", 0))
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{
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}
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DME::~DME ()
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{
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}
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void
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DME::init ()
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{
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string branch;
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branch = "/instrumentation/" + _name;
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SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
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_longitude_node = fgGetNode("/position/longitude-deg", true);
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_latitude_node = fgGetNode("/position/latitude-deg", true);
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_altitude_node = fgGetNode("/position/altitude-ft", true);
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_serviceable_node = node->getChild("serviceable", 0, true);
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_electrical_node = fgGetNode("/systems/electrical/outputs/dme", true);
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SGPropertyNode *fnode = node->getChild("frequencies", 0, true);
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_source_node = fnode->getChild("source", 0, true);
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_frequency_node = fnode->getChild("selected-mhz", 0, true);
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_in_range_node = node->getChild("in-range", 0, true);
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_distance_node = node->getChild("indicated-distance-nm", 0, true);
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_speed_node = node->getChild("indicated-ground-speed-kt", 0, true);
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_time_node = node->getChild("indicated-time-min", 0, true);
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}
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void
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DME::update (double delta_time_sec)
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{
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// Figure out the source
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const char * source = _source_node->getStringValue();
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if (source[0] == '\0') {
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string branch;
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branch = "/instrumentation/" + _name + "/frequencies/selected-mhz";
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_source_node->setStringValue(branch.c_str());
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source = _source_node->getStringValue();
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}
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// Get the frequency
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double frequency_mhz = fgGetDouble(source, 108.0);
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if (frequency_mhz != _last_frequency_mhz) {
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_time_before_search_sec = 0;
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_last_frequency_mhz = frequency_mhz;
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}
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// Get the aircraft position
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double longitude_rad =
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_longitude_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
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double latitude_rad =
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_latitude_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
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double altitude_m =
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_altitude_node->getDoubleValue() * SG_FEET_TO_METER;
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// On timeout, scan again
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_time_before_search_sec -= delta_time_sec;
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if (_time_before_search_sec < 0)
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search(frequency_mhz, longitude_rad,
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latitude_rad, altitude_m);
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// If it's off, don't bother.
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if (!_serviceable_node->getBoolValue() ||
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!_electrical_node->getBoolValue() ||
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!_transmitter_valid) {
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_last_distance_nm = 0;
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_in_range_node->setBoolValue(false);
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_distance_node->setDoubleValue(0);
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_speed_node->setDoubleValue(0);
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_time_node->setDoubleValue(0);
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return;
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}
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// Calculate the distance to the transmitter
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SGGeod geod = SGGeod::fromRadM(longitude_rad, latitude_rad, altitude_m);
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SGVec3d location = SGVec3d::fromGeod(geod);
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double distance_nm = dist(_transmitter, location) * SG_METER_TO_NM;
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double range_nm = adjust_range(_transmitter_elevation_ft,
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altitude_m * SG_METER_TO_FEET,
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_transmitter_range_nm);
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if (distance_nm <= range_nm) {
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double speed_kt = (fabs(distance_nm - _last_distance_nm) *
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((1 / delta_time_sec) * 3600.0));
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_last_distance_nm = distance_nm;
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_in_range_node->setBoolValue(true);
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double tmp_dist = distance_nm - _transmitter_bias;
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if ( tmp_dist < 0.0 ) {
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tmp_dist = 0.0;
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}
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_distance_node->setDoubleValue( tmp_dist );
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_speed_node->setDoubleValue(speed_kt);
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_time_node->setDoubleValue(distance_nm/speed_kt*60.0);
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} else {
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_last_distance_nm = 0;
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_in_range_node->setBoolValue(false);
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_distance_node->setDoubleValue(0);
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_speed_node->setDoubleValue(0);
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_time_node->setDoubleValue(0);
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}
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}
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void
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DME::search (double frequency_mhz, double longitude_rad,
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double latitude_rad, double altitude_m)
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{
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// reset search time
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_time_before_search_sec = 1.0;
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// try the ILS list first
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FGNavRecord *dme = globals->get_dmelist()->findByFreq( frequency_mhz,
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SGGeod::fromRadM(longitude_rad, latitude_rad, altitude_m));
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_transmitter_valid = (dme != NULL);
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if ( _transmitter_valid ) {
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_transmitter = dme->cart();
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_transmitter_elevation_ft = dme->get_elev_ft();
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_transmitter_range_nm = dme->get_range();
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_transmitter_bias = dme->get_multiuse();
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}
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}
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// end of dme.cxx
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