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flightgear/src/Instrumentation/dme.cxx
jmt 45a446dfaf Syd Adams:
add ias-limit (brarber-pole) computation to airpseed-indicator
    expose selected DME frequency on the DME instrument
2010-03-11 08:58:23 +01:00

184 lines
5.8 KiB
C++

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