//
// You should have received a copy of the GNU General Public License
// along with this program; if not, write to the Free Software
-// Foundation, Inc., 675 Mass Ave, Cambridge, MA 02139, USA.
+// Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
//
// $Id$
# include <config.h>
#endif
-#include <iostream>
-#include <string>
+#include "navradio.hxx"
+
#include <sstream>
-#include <simgear/compiler.h>
#include <simgear/sg_inlines.h>
-#include <simgear/math/sg_random.h>
+#include <simgear/timing/sg_time.hxx>
#include <simgear/math/vector.hxx>
+#include <simgear/math/sg_random.h>
+#include <simgear/misc/sg_path.hxx>
+#include <simgear/math/sg_geodesy.hxx>
+#include <simgear/structure/exception.hxx>
+#include <simgear/math/interpolater.hxx>
+
+#include <Navaids/navrecord.hxx>
-#include <Aircraft/aircraft.hxx>
+#include <Airports/runways.hxx>
#include <Navaids/navlist.hxx>
+#include <Main/util.hxx>
-#include "navradio.hxx"
-#include <string>
-SG_USING_STD(string);
+using std::string;
+// General-purpose sawtooth function. Graph looks like this:
+// /\ .
+// \/
+// Odd symmetry, inversion symmetry about the origin.
+// Unit slope at the origin.
+// Max 1, min -1, period 4.
+// Two zero-crossings per period, one with + slope, one with - slope.
+// Useful for false localizer courses.
+static double sawtooth(double xx)
+{
+ return 4.0 * fabs(xx/4.0 + 0.25 - floor(xx/4.0 + 0.75)) - 1.0;
+}
+
+// Calculate a unit vector in the horizontal tangent plane
+// starting at the given "tail" of the vector and going off
+// with the given heading.
+static SGVec3d tangentVector(const SGGeod& tail, const SGVec3d& tail_xyz,
+ const double heading)
+{
+// The fudge factor here is presumably intended to improve
+// numerical stability. I don't know if it is necessary.
+// It gets divided out later.
+ double fudge(100.0);
+ SGGeod head;
+ double az2; // ignored
+ SGGeodesy::direct(tail, heading, fudge, head, az2);
+ head.setElevationM(tail.getElevationM());
+ SGVec3d head_xyz = SGVec3d::fromGeod(head);
+ return (head_xyz - tail_xyz) * (1.0/fudge);
+}
// Constructor
FGNavRadio::FGNavRadio(SGPropertyNode *node) :
power_btn_node(NULL),
freq_node(NULL),
alt_freq_node(NULL),
- fmt_freq_node(NULL),
- fmt_alt_freq_node(NULL),
sel_radial_node(NULL),
vol_btn_node(NULL),
ident_btn_node(NULL),
audio_btn_node(NULL),
+ backcourse_node(NULL),
nav_serviceable_node(NULL),
cdi_serviceable_node(NULL),
gs_serviceable_node(NULL),
tofrom_serviceable_node(NULL),
+ fmt_freq_node(NULL),
+ fmt_alt_freq_node(NULL),
heading_node(NULL),
radial_node(NULL),
recip_radial_node(NULL),
to_flag_node(NULL),
from_flag_node(NULL),
inrange_node(NULL),
+ signal_quality_norm_node(NULL),
cdi_deflection_node(NULL),
+ cdi_deflection_norm_node(NULL),
cdi_xtrack_error_node(NULL),
cdi_xtrack_hdg_err_node(NULL),
has_gs_node(NULL),
loc_node(NULL),
loc_dist_node(NULL),
gs_deflection_node(NULL),
+ gs_deflection_deg_node(NULL),
+ gs_deflection_norm_node(NULL),
gs_rate_of_climb_node(NULL),
gs_dist_node(NULL),
nav_id_node(NULL),
gps_cdi_deflection_node(NULL),
gps_to_flag_node(NULL),
gps_from_flag_node(NULL),
- last_nav_id(""),
- last_nav_vor(false),
+ gps_has_gs_node(NULL),
play_count(0),
last_time(0),
- radial(0.0),
target_radial(0.0),
horiz_vel(0.0),
last_x(0.0),
last_loc_dist(0.0),
last_xtrack_error(0.0),
- name("nav"),
- num(0),
+ _localizerWidth(5.0),
+ _name(node->getStringValue("name", "nav")),
+ _num(node->getIntValue("number", 0)),
_time_before_search_sec(-1.0)
{
SGPath path( globals->get_fg_root() );
term_tbl = new SGInterpTable( term.str() );
low_tbl = new SGInterpTable( low.str() );
high_tbl = new SGInterpTable( high.str() );
-
- int i;
- for ( i = 0; i < node->nChildren(); ++i ) {
- SGPropertyNode *child = node->getChild(i);
- string cname = child->getName();
- string cval = child->getStringValue();
- if ( cname == "name" ) {
- name = cval;
- } else if ( cname == "number" ) {
- num = child->getIntValue();
- } else {
- SG_LOG( SG_INSTR, SG_WARN,
- "Error in nav radio config logic" );
- if ( name.length() ) {
- SG_LOG( SG_INSTR, SG_WARN, "Section = " << name );
- }
- }
- }
-
}
morse.init();
string branch;
- branch = "/instrumentation/" + name;
+ branch = "/instrumentation/" + _name;
- SGPropertyNode *node = fgGetNode(branch.c_str(), num, true );
+ SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
bus_power_node =
- fgGetNode(("/systems/electrical/outputs/" + name).c_str(), true);
+ fgGetNode(("/systems/electrical/outputs/" + _name).c_str(), true);
// inputs
is_valid_node = node->getChild("data-is-valid", 0, true);
ident_btn_node->setBoolValue( true );
audio_btn_node = node->getChild("audio-btn", 0, true);
audio_btn_node->setBoolValue( true );
+ backcourse_node = node->getChild("back-course-btn", 0, true);
+ backcourse_node->setBoolValue( false );
nav_serviceable_node = node->getChild("serviceable", 0, true);
cdi_serviceable_node = (node->getChild("cdi", 0, true))
->getChild("serviceable", 0, true);
to_flag_node = node->getChild("to-flag", 0, true);
from_flag_node = node->getChild("from-flag", 0, true);
inrange_node = node->getChild("in-range", 0, true);
+ signal_quality_norm_node = node->getChild("signal-quality-norm", 0, true);
cdi_deflection_node = node->getChild("heading-needle-deflection", 0, true);
+ cdi_deflection_norm_node = node->getChild("heading-needle-deflection-norm", 0, true);
cdi_xtrack_error_node = node->getChild("crosstrack-error-m", 0, true);
cdi_xtrack_hdg_err_node
= node->getChild("crosstrack-heading-error-deg", 0, true);
loc_node = node->getChild("nav-loc", 0, true);
loc_dist_node = node->getChild("nav-distance", 0, true);
gs_deflection_node = node->getChild("gs-needle-deflection", 0, true);
+ gs_deflection_deg_node = node->getChild("gs-needle-deflection-deg", 0, true);
+ gs_deflection_norm_node = node->getChild("gs-needle-deflection-norm", 0, true);
gs_rate_of_climb_node = node->getChild("gs-rate-of-climb", 0, true);
gs_dist_node = node->getChild("gs-distance", 0, true);
nav_id_node = node->getChild("nav-id", 0, true);
gps_cdi_deflection_node = fgGetNode("/instrumentation/gps/cdi-deflection", true);
gps_to_flag_node = fgGetNode("/instrumentation/gps/to-flag", true);
gps_from_flag_node = fgGetNode("/instrumentation/gps/from-flag", true);
+ gps_has_gs_node = fgGetNode("/instrumentation/gps/has-gs", true);
std::ostringstream temp;
- temp << name << "nav-ident" << num;
+ temp << _name << "nav-ident" << _num;
nav_fx_name = temp.str();
- temp << name << "dme-ident" << num;
+ temp << _name << "dme-ident" << _num;
dme_fx_name = temp.str();
}
{
std::ostringstream temp;
string branch;
- temp << num;
- branch = "/instrumentation/" + name + "[" + temp.str() + "]";
+ temp << _num;
+ branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
}
{
std::ostringstream temp;
string branch;
- temp << num;
- branch = "/instrumentation/" + name + "[" + temp.str() + "]";
+ temp << _num;
+ branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
}
void
FGNavRadio::update(double dt)
{
- // Do a nav station search only once a second to reduce
- // unnecessary work. (Also, make sure to do this before caching
- // any values!)
- _time_before_search_sec -= dt;
- if ( _time_before_search_sec < 0 ) {
- search();
+ if (dt <= 0.0) {
+ return; // paused
+ }
+
+ // Create "formatted" versions of the nav frequencies for
+ // instrument displays.
+ char tmp[16];
+ sprintf( tmp, "%.2f", freq_node->getDoubleValue() );
+ fmt_freq_node->setStringValue(tmp);
+ sprintf( tmp, "%.2f", alt_freq_node->getDoubleValue() );
+ fmt_alt_freq_node->setStringValue(tmp);
+
+ if (power_btn_node->getBoolValue()
+ && (bus_power_node->getDoubleValue() > 1.0)
+ && nav_serviceable_node->getBoolValue() )
+ {
+ if (nav_slaved_to_gps_node->getBoolValue()) {
+ updateGPSSlaved();
+ } else {
+ updateReceiver(dt);
}
+
+ updateCDI(dt);
+ } else {
+ clearOutputs();
+ }
+
+ updateAudio();
+}
- // cache a few strategic values locally for speed
- double lon = lon_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
- double lat = lat_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
- double elev = alt_node->getDoubleValue() * SG_FEET_TO_METER;
- bool power_btn = power_btn_node->getBoolValue();
- bool nav_serviceable = nav_serviceable_node->getBoolValue();
- bool cdi_serviceable = cdi_serviceable_node->getBoolValue();
- bool tofrom_serviceable = tofrom_serviceable_node->getBoolValue();
- bool inrange = inrange_node->getBoolValue();
- bool has_gs = has_gs_node->getBoolValue();
- bool is_loc = loc_node->getBoolValue();
- double loc_dist = loc_dist_node->getDoubleValue();
-
- Point3D aircraft = sgGeodToCart( Point3D( lon, lat, elev ) );
- Point3D station;
- double az1, az2, s;
-
- // Create "formatted" versions of the nav frequencies for
- // instrument displays.
- char tmp[16];
- sprintf( tmp, "%.2f", freq_node->getDoubleValue() );
- fmt_freq_node->setStringValue(tmp);
- sprintf( tmp, "%.2f", alt_freq_node->getDoubleValue() );
- fmt_alt_freq_node->setStringValue(tmp);
-
- // cout << "is_valid = " << is_valid
- // << " power_btn = " << power_btn
- // << " bus_power = " << bus_power_node->getDoubleValue()
- // << " nav_serviceable = " << nav_serviceable
- // << endl;
-
- if ( is_valid && power_btn && (bus_power_node->getDoubleValue() > 1.0)
- && nav_serviceable )
- {
- station = Point3D( nav_x, nav_y, nav_z );
- loc_dist = aircraft.distance3D( station );
- loc_dist_node->setDoubleValue( loc_dist );
- // cout << "station = " << station << " dist = " << loc_dist << endl;
-
- if ( has_gs ) {
- // find closest distance to the gs base line
- sgdVec3 p;
- sgdSetVec3( p, aircraft.x(), aircraft.y(), aircraft.z() );
- sgdVec3 p0;
- sgdSetVec3( p0, gs_x, gs_y, gs_z );
- double dist = sgdClosestPointToLineDistSquared( p, p0,
- gs_base_vec );
- gs_dist_node->setDoubleValue( sqrt( dist ) );
- // cout << "gs_dist = " << gs_dist_node->getDoubleValue()
- // << endl;
-
- Point3D tmp( gs_x, gs_y, gs_z );
- // cout << " (" << aircraft.distance3D( tmp ) << ")" << endl;
-
- // wgs84 heading to glide slope (to determine sign of distance)
- geo_inverse_wgs_84( elev,
- lat * SGD_RADIANS_TO_DEGREES,
- lon * SGD_RADIANS_TO_DEGREES,
- gs_lat, gs_lon,
- &az1, &az2, &s );
- double r = az1 - target_radial;
- while ( r > 180.0 ) { r -= 360.0;}
- while ( r < -180.0 ) { r += 360.0;}
- if ( r >= -90.0 && r <= 90.0 ) {
- gs_dist_signed = gs_dist_node->getDoubleValue();
- } else {
- gs_dist_signed = -gs_dist_node->getDoubleValue();
- }
- /* cout << "Target Radial = " << target_radial
- << " Bearing = " << az1
- << " dist (signed) = " << gs_dist_signed
- << endl; */
-
- } else {
- gs_dist_node->setDoubleValue( 0.0 );
- }
-
- //////////////////////////////////////////////////////////
+void FGNavRadio::clearOutputs()
+{
+ inrange_node->setBoolValue( false );
+ cdi_deflection_node->setDoubleValue( 0.0 );
+ cdi_deflection_norm_node->setDoubleValue( 0.0 );
+ cdi_xtrack_error_node->setDoubleValue( 0.0 );
+ cdi_xtrack_hdg_err_node->setDoubleValue( 0.0 );
+ time_to_intercept->setDoubleValue( 0.0 );
+ gs_deflection_node->setDoubleValue( 0.0 );
+ gs_deflection_deg_node->setDoubleValue(0.0);
+ gs_deflection_norm_node->setDoubleValue(0.0);
+
+ to_flag_node->setBoolValue( false );
+ from_flag_node->setBoolValue( false );
+}
+
+void FGNavRadio::updateReceiver(double dt)
+{
+ // Do a nav station search only once a second to reduce
+ // unnecessary work. (Also, make sure to do this before caching
+ // any values!)
+ _time_before_search_sec -= dt;
+ if ( _time_before_search_sec < 0 ) {
+ search();
+ }
+
+ if (!_navaid) {
+ _cdiDeflection = 0.0;
+ _cdiCrossTrackErrorM = 0.0;
+ _toFlag = _fromFlag = false;
+ _gsNeedleDeflection = 0.0;
+ _gsNeedleDeflectionNorm = 0.0;
+ inrange_node->setBoolValue(false);
+ return;
+ }
+
+ SGGeod pos = SGGeod::fromDegFt(lon_node->getDoubleValue(),
+ lat_node->getDoubleValue(),
+ alt_node->getDoubleValue());
+
+ double nav_elev = _navaid->get_elev_ft();
+ SGVec3d aircraft = SGVec3d::fromGeod(pos);
+ double loc_dist = dist(aircraft, _navaid->cart());
+ loc_dist_node->setDoubleValue( loc_dist );
+ bool is_loc = loc_node->getBoolValue();
+ double signal_quality_norm = signal_quality_norm_node->getDoubleValue();
+
+ double az2, s;
+ //////////////////////////////////////////////////////////
// compute forward and reverse wgs84 headings to localizer
- //////////////////////////////////////////////////////////
- double hdg;
- geo_inverse_wgs_84( elev,
- lat * SGD_RADIANS_TO_DEGREES,
- lon * SGD_RADIANS_TO_DEGREES,
- loc_lat, loc_lon,
- &hdg, &az2, &s );
- // cout << "az1 = " << az1 << " magvar = " << nav_magvar << endl;
- heading_node->setDoubleValue( hdg );
- radial = az2 - twist;
- double recip = radial + 180.0;
- if ( recip >= 360.0 ) { recip -= 360.0; }
- radial_node->setDoubleValue( radial );
- recip_radial_node->setDoubleValue( recip );
- // cout << " heading = " << heading_node->getDoubleValue()
- // << " dist = " << nav_dist << endl;
-
- //////////////////////////////////////////////////////////
- // compute the target/selected radial in "true" heading
- //////////////////////////////////////////////////////////
- double trtrue = 0.0;
- if ( is_loc ) {
- // ILS localizers radials are already "true" in our
- // database
- trtrue = target_radial;
- } else {
- // VOR radials need to have that vor's offset added in
- trtrue = target_radial + twist;
- }
-
- while ( trtrue < 0.0 ) { trtrue += 360.0; }
- while ( trtrue > 360.0 ) { trtrue -= 360.0; }
- target_radial_true_node->setDoubleValue( trtrue );
-
- //////////////////////////////////////////////////////////
- // adjust reception range for altitude
- //////////////////////////////////////////////////////////
+ //////////////////////////////////////////////////////////
+ double hdg;
+ SGGeodesy::inverse(pos, _navaid->geod(), hdg, az2, s);
+ heading_node->setDoubleValue(hdg);
+ double radial = az2 - twist;
+ double recip = radial + 180.0;
+ SG_NORMALIZE_RANGE(recip, 0.0, 360.0);
+ radial_node->setDoubleValue( radial );
+ recip_radial_node->setDoubleValue( recip );
+
+ //////////////////////////////////////////////////////////
+ // compute the target/selected radial in "true" heading
+ //////////////////////////////////////////////////////////
+ if (!is_loc) {
+ target_radial = sel_radial_node->getDoubleValue();
+ }
+
+ // VORs need twist (mag-var) added; ILS/LOCs don't but we set twist to 0.0
+ double trtrue = target_radial + twist;
+ SG_NORMALIZE_RANGE(trtrue, 0.0, 360.0);
+ target_radial_true_node->setDoubleValue( trtrue );
+
+ //////////////////////////////////////////////////////////
+ // adjust reception range for altitude
+ // FIXME: make sure we are using the navdata range now that
+ // it is valid in the data file
+ //////////////////////////////////////////////////////////
if ( is_loc ) {
double offset = radial - target_radial;
- while ( offset < -180.0 ) { offset += 360.0; }
- while ( offset > 180.0 ) { offset -= 360.0; }
- // cout << "ils offset = " << offset << endl;
+ SG_NORMALIZE_RANGE(offset, -180.0, 180.0);
effective_range
- = adjustILSRange( nav_elev, elev, offset,
+ = adjustILSRange( nav_elev, pos.getElevationM(), offset,
loc_dist * SG_METER_TO_NM );
} else {
- effective_range = adjustNavRange( nav_elev, elev, range );
- }
- // cout << "nav range = " << effective_range
- // << " (" << range << ")" << endl;
-
- if ( loc_dist < effective_range * SG_NM_TO_METER ) {
- inrange = true;
- } else if ( loc_dist < 2 * effective_range * SG_NM_TO_METER ) {
- inrange = sg_random() < ( 2 * effective_range * SG_NM_TO_METER
- - loc_dist )
- / (effective_range * SG_NM_TO_METER);
- } else {
- inrange = false;
+ effective_range
+ = adjustNavRange( nav_elev, pos.getElevationM(), _navaid->get_range() );
}
- inrange_node->setBoolValue( inrange );
- if ( !is_loc ) {
- target_radial = sel_radial_node->getDoubleValue();
- }
+ double effective_range_m = effective_range * SG_NM_TO_METER;
+
+ //////////////////////////////////////////////////////////
+ // compute signal quality
+ // 100% within effective_range
+ // decreases 1/x^2 further out
+ //////////////////////////////////////////////////////////
+ double last_signal_quality_norm = signal_quality_norm;
+
+ if ( loc_dist < effective_range_m ) {
+ signal_quality_norm = 1.0;
+ } else {
+ double range_exceed_norm = loc_dist/effective_range_m;
+ signal_quality_norm = 1/(range_exceed_norm*range_exceed_norm);
+ }
+
+ signal_quality_norm = fgGetLowPass( last_signal_quality_norm,
+ signal_quality_norm, dt );
+
+ signal_quality_norm_node->setDoubleValue( signal_quality_norm );
+ bool inrange = signal_quality_norm > 0.2;
+ inrange_node->setBoolValue( inrange );
+
+ //////////////////////////////////////////////////////////
+ // compute to/from flag status
+ //////////////////////////////////////////////////////////
+ if (inrange) {
+ if (is_loc) {
+ _toFlag = true;
+ } else {
+ double offset = fabs(radial - target_radial);
+ _toFlag = (offset > 90.0 && offset < 270.0);
+ }
+ _fromFlag = !_toFlag;
+ } else {
+ _toFlag = _fromFlag = false;
+ }
+
+ // CDI deflection
+ double r = target_radial - radial;
+ SG_NORMALIZE_RANGE(r, -180.0, 180.0);
+
+ if ( is_loc ) {
+ // The factor of 30.0 gives a period of 120 which gives us 3 cycles and six
+ // zeros i.e. six courses: one front course, one back course, and four
+ // false courses. Three of the six are reverse sensing.
+ _cdiDeflection = 30.0 * sawtooth(r / 30.0);
+ const double VOR_FULL_ARC = 20.0; // VOR is -10 .. 10 degree swing
+ _cdiDeflection *= VOR_FULL_ARC / _localizerWidth; // increased localiser sensitivity
+ } else {
+ // handle the TO side of the VOR
+ if (fabs(r) > 90.0) {
+ r = ( r<0.0 ? -r-180.0 : -r+180.0 );
+ }
+ _cdiDeflection = r;
+ } // of non-localiser case
+
+ SG_CLAMP_RANGE(_cdiDeflection, -10.0, 10.0 );
+ _cdiDeflection *= signal_quality_norm;
+
+ // cross-track error (in metres)
+ _cdiCrossTrackErrorM = loc_dist * sin(r * SGD_DEGREES_TO_RADIANS);
+
+ updateGlideSlope(dt, aircraft, signal_quality_norm);
+
+ last_loc_dist = loc_dist;
+}
- //////////////////////////////////////////////////////////
- // compute to/from flag status
- //////////////////////////////////////////////////////////
- double value = false;
- double offset = fabs(radial - target_radial);
- if ( tofrom_serviceable ) {
- if ( nav_slaved_to_gps_node->getBoolValue() ) {
- value = gps_to_flag_node->getBoolValue();
- } else if ( inrange ) {
- if ( is_loc ) {
- value = true;
- } else {
- value = !(offset <= 90.0 || offset >= 270.0);
- }
- }
- } else {
- value = false;
- }
- to_flag_node->setBoolValue( value );
-
- value = false;
- if ( tofrom_serviceable ) {
- if ( nav_slaved_to_gps_node->getBoolValue() ) {
- value = gps_from_flag_node->getBoolValue();
- } else if ( inrange ) {
- if ( is_loc ) {
- value = false;
- } else {
- value = !(offset > 90.0 && offset < 270.0);
- }
- }
- } else {
- value = false;
- }
- from_flag_node->setBoolValue( value );
-
- //////////////////////////////////////////////////////////
- // compute the deflection of the CDI needle, clamped to the range
- // of ( -10 , 10 )
- //////////////////////////////////////////////////////////
- double r = 0.0;
- if ( cdi_serviceable ) {
- if ( nav_slaved_to_gps_node->getBoolValue() ) {
- r = gps_cdi_deflection_node->getDoubleValue();
- // We want +- 5 dots deflection for the gps, so clamp
- // to -12.5/12.5
- if ( r < -12.5 ) { r = -12.5; }
- if ( r > 12.5 ) { r = 12.5; }
- } else if ( inrange ) {
- r = radial - target_radial;
- // cout << "Target radial = " << target_radial
- // << " Actual radial = " << radial << endl;
-
- while ( r > 180.0 ) { r -= 360.0;}
- while ( r < -180.0 ) { r += 360.0;}
- if ( fabs(r) > 90.0 ) {
- r = ( r<0.0 ? -r-180.0 : -r+180.0 );
- }
-
- // According to Robin Peel, the ILS is 4x more
- // sensitive than a vor
- r = -r; // reverse, since radial is outbound
- if ( is_loc ) { r *= 4.0; }
- if ( r < -10.0 ) { r = -10.0; }
- if ( r > 10.0 ) { r = 10.0; }
- }
- }
- cdi_deflection_node->setDoubleValue( r );
-
- //////////////////////////////////////////////////////////
- // compute the amount of cross track distance error in meters
- //////////////////////////////////////////////////////////
- double xtrack_error = 0.0;
- if ( inrange && nav_serviceable && cdi_serviceable ) {
- r = radial - target_radial;
- // cout << "Target radial = " << target_radial
- // << " Actual radial = " << radial
- // << " r = " << r << endl;
+void FGNavRadio::updateGlideSlope(double dt, const SGVec3d& aircraft, double signal_quality_norm)
+{
+ _gsNeedleDeflection = 0.0;
+ if (!_gs || !inrange_node->getBoolValue()) {
+ gs_dist_node->setDoubleValue( 0.0 );
+ return;
+ }
+
+ double gsDist = dist(aircraft, _gsCart);
+ gs_dist_node->setDoubleValue(gsDist);
+ if (gsDist > (_gs->get_range() * SG_NM_TO_METER)) {
+ return;
+ }
+
+ SGVec3d pos = aircraft - _gsCart; // relative vector from gs antenna to aircraft
+ // The positive GS axis points along the runway in the landing direction,
+ // toward the far end, not toward the approach area, so we need a - sign here:
+ double dot_h = -dot(pos, _gsAxis);
+ double dot_v = dot(pos, _gsVertical);
+ double angle = atan2(dot_v, dot_h) * SGD_RADIANS_TO_DEGREES;
+ double deflectionAngle = target_gs - angle;
- while ( r > 180.0 ) { r -= 360.0;}
- while ( r < -180.0 ) { r += 360.0;}
- if ( fabs(r) > 90.0 ) {
- r = ( r<0.0 ? -r-180.0 : -r+180.0 );
- }
-
- r = -r; // reverse, since radial is outbound
-
- xtrack_error = loc_dist * sin(r * SGD_DEGREES_TO_RADIANS);
- } else {
- xtrack_error = 0.0;
- }
- cdi_xtrack_error_node->setDoubleValue( xtrack_error );
-
- //////////////////////////////////////////////////////////
- // compute an approximate ground track heading error
- //////////////////////////////////////////////////////////
- double hdg_error = 0.0;
- if ( inrange && cdi_serviceable ) {
- double ddist = last_loc_dist - loc_dist;
- double dxtrack = last_xtrack_error - xtrack_error;
- double a = atan2( dxtrack, ddist ) * SGD_RADIANS_TO_DEGREES;
- if ( from_flag_node->getBoolValue() ) {
- a = 180.0 - a;
- if ( a > 180.0 ) { a -= 360.0; }
- if ( a < -180.0 ) { a += 360.0; }
- }
- SGPropertyNode *true_hdg
- = fgGetNode("/orientation/heading-deg", true);
- // cout << "true heading = " << true_hdg->getDoubleValue()
- // << " selrad = " << sel_radial_node->getDoubleValue()
- // << " artr = " << a
- // << endl;
- double est_hdg = trtrue + a;
- if ( est_hdg < 0.0 ) { est_hdg += 360.0; }
- if ( est_hdg >= 360.0 ) { est_hdg -= 360.0; }
- hdg_error = est_hdg - true_hdg->getDoubleValue();
- }
- cdi_xtrack_hdg_err_node->setDoubleValue( hdg_error );
-
- //////////////////////////////////////////////////////////
- // compute the time to intercept selected radial (based on
- // current and last cross track errors and dt
- //////////////////////////////////////////////////////////
- double t = 0.0;
- if ( inrange && cdi_serviceable ) {
- double xrate_ms = (last_xtrack_error - xtrack_error) / dt;
- if ( fabs(xrate_ms) > 0.00001 ) {
- t = xtrack_error / xrate_ms;
- } else {
- t = 9999.9;
- }
- }
- time_to_intercept->setDoubleValue( t );
-
- //////////////////////////////////////////////////////////
- // compute the amount of glide slope needle deflection
- // (.i.e. the number of degrees we are off the glide slope * 5.0
- //////////////////////////////////////////////////////////
- r = 0.0;
- if ( has_gs && gs_serviceable_node->getBoolValue() ) {
- if ( nav_slaved_to_gps_node->getBoolValue() ) {
- // FIXME/FINISHME, what should be set here?
- } else if ( inrange ) {
- double x = gs_dist_node->getDoubleValue();
- double y = (fgGetDouble("/position/altitude-ft") - nav_elev)
- * SG_FEET_TO_METER;
- // cout << "dist = " << x << " height = " << y << endl;
- double angle = asin( y / x ) * SGD_RADIANS_TO_DEGREES;
- r = (target_gs - angle) * 5.0;
- }
- }
- gs_deflection_node->setDoubleValue( r );
-
- //////////////////////////////////////////////////////////
- // Calculate desired rate of climb for intercepting the GS
- //////////////////////////////////////////////////////////
- double x = gs_dist_node->getDoubleValue();
- double y = (alt_node->getDoubleValue() - nav_elev)
- * SG_FEET_TO_METER;
- double current_angle = atan2( y, x ) * SGD_RADIANS_TO_DEGREES;
-
- double target_angle = target_gs;
- double gs_diff = target_angle - current_angle;
-
- // convert desired vertical path angle into a climb rate
- double des_angle = current_angle - 10 * gs_diff;
-
- // estimate horizontal speed towards ILS in meters per minute
- double dist = last_x - x;
- last_x = x;
- if ( dt > 0.0 ) {
- // avoid nan
- double new_vel = ( dist / dt );
+ // Construct false glideslopes. The scale factor of 1.5
+ // in the sawtooth gives a period of 6 degrees.
+ // There will be zeros at 3, 6r, 9, 12r et cetera
+ // where "r" indicates reverse sensing.
+ // This is is consistent with conventional pilot lore
+ // e.g. http://www.allstar.fiu.edu/aerojava/ILS.htm
+ // but inconsistent with
+ // http://www.freepatentsonline.com/3757338.html
+ //
+ // It may be that some of each exist.
+ if (deflectionAngle < 0) {
+ deflectionAngle = 1.5 * sawtooth(deflectionAngle / 1.5);
+ } else {
+ // no false GS below the true GS
+ }
+
+ _gsNeedleDeflection = deflectionAngle * 5.0;
+ _gsNeedleDeflection *= signal_quality_norm;
+
+ SG_CLAMP_RANGE(deflectionAngle, -0.7, 0.7);
+ _gsNeedleDeflectionNorm = (deflectionAngle / 0.7) * signal_quality_norm;
+
+ //////////////////////////////////////////////////////////
+ // Calculate desired rate of climb for intercepting the GS
+ //////////////////////////////////////////////////////////
+ double gs_diff = target_gs - angle;
+ // convert desired vertical path angle into a climb rate
+ double des_angle = angle - 10 * gs_diff;
+
+ // estimate horizontal speed towards ILS in meters per minute
+ double elapsedDistance = last_x - gsDist;
+ last_x = gsDist;
+
+ double new_vel = ( elapsedDistance / dt );
+ horiz_vel = 0.75 * horiz_vel + 0.25 * new_vel;
+
+ gs_rate_of_climb_node
+ ->setDoubleValue( -sin( des_angle * SGD_DEGREES_TO_RADIANS )
+ * horiz_vel * SG_METER_TO_FEET );
+}
+
+void FGNavRadio::updateGPSSlaved()
+{
+ has_gs_node->setBoolValue(gps_has_gs_node->getBoolValue());
- horiz_vel = 0.75 * horiz_vel + 0.25 * new_vel;
- // double horiz_vel = cur_fdm_state->get_V_ground_speed()
- // * SG_FEET_TO_METER * 60.0;
- // double horiz_vel = airspeed_node->getFloatValue()
- // * SG_FEET_TO_METER * 60.0;
-
- gs_rate_of_climb_node
- ->setDoubleValue( -sin( des_angle * SGD_DEGREES_TO_RADIANS )
- * horiz_vel * SG_METER_TO_FEET );
- }
-
- //////////////////////////////////////////////////////////
- // Calculate a suggested target heading to smoothly intercept
- // a nav/ils radial.
- //////////////////////////////////////////////////////////
-
- // FIXME: this smells odd, there must be a better (or more
- // linear) solution
- //
- // determine the heading adjustment needed.
- // over 8km scale by 3.0
- // (3 is chosen because max deflection is 10
- // and 30 is clamped angle to radial)
- // under 8km scale by 10.0
- // because the overstated error helps drive it to the radial in a
- // moderate cross wind.
- double adjustment = 0.0;
- if ( loc_dist > 8000 ) {
- adjustment = cdi_deflection_node->getDoubleValue() * 3.0;
- } else {
- adjustment = cdi_deflection_node->getDoubleValue() * 10.0;
- }
- SG_CLAMP_RANGE( adjustment, -30.0, 30.0 );
-
- // determine the target heading to fly to intercept the
- // tgt_radial = target radial (true) + cdi offset adjustmest -
- // xtrack heading error adjustment
- double nta_hdg = trtrue + adjustment - hdg_error;
- while ( nta_hdg < 0.0 ) { nta_hdg += 360.0; }
- while ( nta_hdg > 360.0 ) { nta_hdg -= 360.0; }
- target_auto_hdg_node->setDoubleValue( nta_hdg );
-
- last_xtrack_error = xtrack_error;
- } else {
- inrange_node->setBoolValue( false );
- cdi_deflection_node->setDoubleValue( 0.0 );
- cdi_xtrack_error_node->setDoubleValue( 0.0 );
- cdi_xtrack_hdg_err_node->setDoubleValue( 0.0 );
- time_to_intercept->setDoubleValue( 0.0 );
- gs_deflection_node->setDoubleValue( 0.0 );
- to_flag_node->setBoolValue( false );
- from_flag_node->setBoolValue( false );
- // cout << "not picking up vor. :-(" << endl;
+ _toFlag = gps_to_flag_node->getBoolValue();
+ _fromFlag = gps_from_flag_node->getBoolValue();
+
+ inrange_node->setBoolValue(_toFlag | _fromFlag);
+
+ _cdiDeflection = gps_cdi_deflection_node->getDoubleValue();
+ // clmap to some range (+/- 10 degrees) as the regular deflection
+ SG_CLAMP_RANGE(_cdiDeflection, -10.0, 10.0 );
+
+ _cdiCrossTrackErrorM = 0.0; // FIXME, supply this
+ _gsNeedleDeflection = 0.0; // FIXME, supply this
+}
+
+void FGNavRadio::updateCDI(double dt)
+{
+ bool cdi_serviceable = cdi_serviceable_node->getBoolValue();
+ bool inrange = inrange_node->getBoolValue();
+
+ if (tofrom_serviceable_node->getBoolValue()) {
+ to_flag_node->setBoolValue(_toFlag);
+ from_flag_node->setBoolValue(_fromFlag);
+ } else {
+ to_flag_node->setBoolValue(false);
+ from_flag_node->setBoolValue(false);
+ }
+
+ if (!cdi_serviceable) {
+ _cdiDeflection = 0.0;
+ _cdiCrossTrackErrorM = 0.0;
+ }
+
+ cdi_deflection_node->setDoubleValue(_cdiDeflection);
+ cdi_deflection_norm_node->setDoubleValue(_cdiDeflection * 0.1);
+ cdi_xtrack_error_node->setDoubleValue(_cdiCrossTrackErrorM);
+
+ //////////////////////////////////////////////////////////
+ // compute an approximate ground track heading error
+ //////////////////////////////////////////////////////////
+ double hdg_error = 0.0;
+ if ( inrange && cdi_serviceable ) {
+ double vn = fgGetDouble( "/velocities/speed-north-fps" );
+ double ve = fgGetDouble( "/velocities/speed-east-fps" );
+ double gnd_trk_true = atan2( ve, vn ) * SGD_RADIANS_TO_DEGREES;
+ if ( gnd_trk_true < 0.0 ) { gnd_trk_true += 360.0; }
+
+ SGPropertyNode *true_hdg
+ = fgGetNode("/orientation/heading-deg", true);
+ hdg_error = gnd_trk_true - true_hdg->getDoubleValue();
+
+ // cout << "ground track = " << gnd_trk_true
+ // << " orientation = " << true_hdg->getDoubleValue() << endl;
+ }
+ cdi_xtrack_hdg_err_node->setDoubleValue( hdg_error );
+
+ //////////////////////////////////////////////////////////
+ // Calculate a suggested target heading to smoothly intercept
+ // a nav/ils radial.
+ //////////////////////////////////////////////////////////
+
+ // Now that we have cross track heading adjustment built in,
+ // we shouldn't need to overdrive the heading angle within 8km
+ // of the station.
+ //
+ // The cdi deflection should be +/-10 for a full range of deflection
+ // so multiplying this by 3 gives us +/- 30 degrees heading
+ // compensation.
+ double adjustment = _cdiDeflection * 3.0;
+ SG_CLAMP_RANGE( adjustment, -30.0, 30.0 );
+
+ // determine the target heading to fly to intercept the
+ // tgt_radial = target radial (true) + cdi offset adjustmest -
+ // xtrack heading error adjustment
+ double nta_hdg;
+ double trtrue = target_radial_true_node->getDoubleValue();
+ if ( loc_node->getBoolValue() && backcourse_node->getBoolValue() ) {
+ // tuned to a localizer and backcourse mode activated
+ trtrue += 180.0; // reverse the target localizer heading
+ SG_NORMALIZE_RANGE(trtrue, 0.0, 360.0);
+ nta_hdg = trtrue - adjustment - hdg_error;
+ } else {
+ nta_hdg = trtrue + adjustment - hdg_error;
+ }
+
+ SG_NORMALIZE_RANGE(nta_hdg, 0.0, 360.0);
+ target_auto_hdg_node->setDoubleValue( nta_hdg );
+
+ //////////////////////////////////////////////////////////
+ // compute the time to intercept selected radial (based on
+ // current and last cross track errors and dt
+ //////////////////////////////////////////////////////////
+ double t = 0.0;
+ if ( inrange && cdi_serviceable ) {
+ double xrate_ms = (last_xtrack_error - _cdiCrossTrackErrorM) / dt;
+ if ( fabs(xrate_ms) > 0.00001 ) {
+ t = _cdiCrossTrackErrorM / xrate_ms;
+ } else {
+ t = 9999.9;
}
+ }
+ time_to_intercept->setDoubleValue( t );
+
+ if (!gs_serviceable_node->getBoolValue() ) {
+ _gsNeedleDeflection = 0.0;
+ _gsNeedleDeflectionNorm = 0.0;
+ }
+ gs_deflection_node->setDoubleValue(_gsNeedleDeflection);
+ gs_deflection_deg_node->setDoubleValue(_gsNeedleDeflectionNorm * 0.7);
+ gs_deflection_norm_node->setDoubleValue(_gsNeedleDeflectionNorm);
+
+ last_xtrack_error = _cdiCrossTrackErrorM;
+}
- // audio effects
- if ( is_valid && inrange && nav_serviceable ) {
+void FGNavRadio::updateAudio()
+{
+ if (!_navaid || !inrange_node->getBoolValue() || !nav_serviceable_node->getBoolValue()) {
+ return;
+ }
+
// play station ident via audio system if on + ident,
// otherwise turn it off
- if ( power_btn
- && (bus_power_node->getDoubleValue() > 1.0)
- && ident_btn_node->getBoolValue()
- && audio_btn_node->getBoolValue() )
- {
- SGSoundSample *sound;
- sound = globals->get_soundmgr()->find( nav_fx_name );
- double vol = vol_btn_node->getDoubleValue();
- if ( vol < 0.0 ) { vol = 0.0; }
- if ( vol > 1.0 ) { vol = 1.0; }
- if ( sound != NULL ) {
- sound->set_volume( vol );
- } else {
- SG_LOG( SG_COCKPIT, SG_ALERT,
- "Can't find nav-vor-ident sound" );
- }
- sound = globals->get_soundmgr()->find( dme_fx_name );
- if ( sound != NULL ) {
- sound->set_volume( vol );
- } else {
- SG_LOG( SG_COCKPIT, SG_ALERT,
- "Can't find nav-dme-ident sound" );
- }
- // cout << "last_time = " << last_time << " ";
- // cout << "cur_time = "
- // << globals->get_time_params()->get_cur_time();
- if ( last_time <
- globals->get_time_params()->get_cur_time() - 30 ) {
+ if (!power_btn_node->getBoolValue()
+ || !(bus_power_node->getDoubleValue() > 1.0)
+ || !ident_btn_node->getBoolValue()
+ || !audio_btn_node->getBoolValue() ) {
+ globals->get_soundmgr()->stop( nav_fx_name );
+ globals->get_soundmgr()->stop( dme_fx_name );
+ return;
+ }
+
+ SGSoundSample *sound = globals->get_soundmgr()->find( nav_fx_name );
+ double vol = vol_btn_node->getDoubleValue();
+ SG_CLAMP_RANGE(vol, 0.0, 1.0);
+
+ if ( sound != NULL ) {
+ sound->set_volume( vol );
+ } else {
+ SG_LOG( SG_COCKPIT, SG_ALERT, "Can't find nav-vor-ident sound" );
+ }
+
+ sound = globals->get_soundmgr()->find( dme_fx_name );
+ if ( sound != NULL ) {
+ sound->set_volume( vol );
+ } else {
+ SG_LOG( SG_COCKPIT, SG_ALERT, "Can't find nav-dme-ident sound" );
+ }
+
+ if ( last_time < globals->get_time_params()->get_cur_time() - 30 ) {
last_time = globals->get_time_params()->get_cur_time();
play_count = 0;
- }
- // cout << " play_count = " << play_count << endl;
- // cout << "playing = "
- // << globals->get_soundmgr()->is_playing(nav_fx_name)
- // << endl;
- if ( play_count < 4 ) {
+ }
+
+ if ( play_count < 4 ) {
// play VOR ident
if ( !globals->get_soundmgr()->is_playing(nav_fx_name) ) {
globals->get_soundmgr()->play_once( nav_fx_name );
++play_count;
- }
- } else if ( play_count < 5 && has_dme ) {
+ }
+ } else if ( play_count < 5 && has_dme) {
// play DME ident
if ( !globals->get_soundmgr()->is_playing(nav_fx_name) &&
!globals->get_soundmgr()->is_playing(dme_fx_name) ) {
globals->get_soundmgr()->play_once( dme_fx_name );
++play_count;
}
- }
- } else {
- globals->get_soundmgr()->stop( nav_fx_name );
- globals->get_soundmgr()->stop( dme_fx_name );
- }
- }
-
- last_loc_dist = loc_dist;
+ }
}
+FGNavRecord* FGNavRadio::findPrimaryNavaid(const SGGeod& aPos, double aFreqMHz)
+{
+ FGNavRecord* nav = globals->get_navlist()->findByFreq(aFreqMHz, aPos);
+ if (nav) {
+ return nav;
+ }
+
+ return globals->get_loclist()->findByFreq(aFreqMHz, aPos);
+}
// Update current nav/adf radio stations based on current postition
void FGNavRadio::search()
{
+ _time_before_search_sec = 1.0;
+ SGGeod pos = SGGeod::fromDegFt(lon_node->getDoubleValue(),
+ lat_node->getDoubleValue(), alt_node->getDoubleValue());
+ double freq = freq_node->getDoubleValue();
+
+ FGNavRecord* nav = findPrimaryNavaid(pos, freq);
+ if (nav == _navaid) {
+ return; // found the same as last search, we're done
+ }
+
+ _navaid = nav;
+ char identBuffer[5] = " ";
+ if (nav) {
+ FGNavRecord* dme = globals->get_dmelist()->findByFreq(freq, pos);
+ has_dme = (dme != NULL);
+
+ nav_id_node->setStringValue(nav->get_ident());
+ strncpy(identBuffer, nav->ident().c_str(), 5);
+
+ effective_range = adjustNavRange(nav->get_elev_ft(), pos.getElevationM(), nav->get_range());
+ loc_node->setBoolValue(nav->type() != FGPositioned::VOR);
+ twist = nav->get_multiuse();
+
+ if (nav->type() == FGPositioned::VOR) {
+ target_radial = sel_radial_node->getDoubleValue();
+ _gs = NULL;
+ } else { // ILS or LOC
+ _gs = globals->get_gslist()->findByFreq(freq, pos);
+ _localizerWidth = localizerWidth(nav);
+ has_gs_node->setBoolValue(_gs != NULL);
+ twist = 0.0;
+ effective_range = nav->get_range();
+
+ target_radial = nav->get_multiuse();
+ SG_NORMALIZE_RANGE(target_radial, 0.0, 360.0);
+
+ if (_gs) {
+ int tmp = (int)(_gs->get_multiuse() / 1000.0);
+ target_gs = (double)tmp / 100.0;
+
+ // GS axis unit tangent vector
+ // (along the runway)
+ _gsCart = _gs->cart();
+ _gsAxis = tangentVector(_gs->geod(), _gsCart, target_radial);
+
+ // GS baseline unit tangent vector
+ // (perpendicular to the runay along the ground)
+ SGVec3d baseline = tangentVector(_gs->geod(), _gsCart, target_radial + 90.0);
+ _gsVertical = cross(baseline, _gsAxis);
+ } // of have glideslope
+ } // of found LOC or ILS
+
+ audioNavidChanged();
+ } else { // found nothing
+ _gs = NULL;
+ nav_id_node->setStringValue("");
+ has_dme = false;
+ globals->get_soundmgr()->remove( nav_fx_name );
+ globals->get_soundmgr()->remove( dme_fx_name );
+ }
+
+ is_valid_node->setBoolValue(nav != NULL);
+ id_c1_node->setIntValue( (int)identBuffer[0] );
+ id_c2_node->setIntValue( (int)identBuffer[1] );
+ id_c3_node->setIntValue( (int)identBuffer[2] );
+ id_c4_node->setIntValue( (int)identBuffer[3] );
+}
- // reset search time
- _time_before_search_sec = 1.0;
-
- // cache values locally for speed
- double lon = lon_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
- double lat = lat_node->getDoubleValue() * SGD_DEGREES_TO_RADIANS;
- double elev = alt_node->getDoubleValue() * SG_FEET_TO_METER;
-
- FGNavRecord *nav = NULL;
- FGNavRecord *loc = NULL;
- FGNavRecord *dme = NULL;
- FGNavRecord *gs = NULL;
-
- ////////////////////////////////////////////////////////////////////////
- // Nav.
- ////////////////////////////////////////////////////////////////////////
-
- double freq = freq_node->getDoubleValue();
- nav = globals->get_navlist()->findByFreq(freq, lon, lat, elev);
- dme = globals->get_dmelist()->findByFreq(freq, lon, lat, elev);
- if ( nav == NULL ) {
- loc = globals->get_loclist()->findByFreq(freq, lon, lat, elev);
- gs = globals->get_gslist()->findByFreq(freq, lon, lat, elev);
- }
+double FGNavRadio::localizerWidth(FGNavRecord* aLOC)
+{
+ FGRunway* rwy = aLOC->runway();
+ assert(rwy);
+
+ SGVec3d thresholdCart(SGVec3d::fromGeod(rwy->threshold()));
+ double axisLength = dist(aLOC->cart(), thresholdCart);
+ double landingLength = dist(thresholdCart, SGVec3d::fromGeod(rwy->end()));
+
+// Reference: http://dcaa.slv.dk:8000/icaodocs/
+// ICAO standard width at threshold is 210 m = 689 feet = approx 700 feet.
+// ICAO 3.1.1 half course = DDM = 0.0775
+// ICAO 3.1.3.7.1 Sensitivity 0.00145 DDM/m at threshold
+// implies peg-to-peg of 214 m ... we will stick with 210.
+// ICAO 3.1.3.7.1 "Course sector angle shall not exceed 6 degrees."
+
+// Very short runway: less than 1200 m (4000 ft) landing length:
+ if (landingLength < 1200.0) {
+// ICAO fudges localizer sensitivity for very short runways.
+// This produces a non-monotonic sensitivity-versus length relation.
+ axisLength += 1050.0;
+ }
+
+// Example: very short: San Diego KMYF (Montgomery Field) ILS RWY 28R
+// Example: short: Tom's River KMJX (Robert J. Miller) ILS RWY 6
+// Example: very long: Denver KDEN (Denver) ILS RWY 16R
+ double raw_width = 210.0 / axisLength * SGD_RADIANS_TO_DEGREES;
+ return raw_width < 6.0? raw_width : 6.0;
+}
- string nav_id = "";
-
- if ( loc != NULL ) {
- nav_id = loc->get_ident();
- nav_id_node->setStringValue( nav_id.c_str() );
- // cout << "localizer = " << nav_id_node->getStringValue() << endl;
- is_valid = true;
- if ( last_nav_id != nav_id || last_nav_vor ) {
- trans_ident = loc->get_trans_ident();
- target_radial = loc->get_multiuse();
- while ( target_radial < 0.0 ) { target_radial += 360.0; }
- while ( target_radial > 360.0 ) { target_radial -= 360.0; }
- loc_lon = loc->get_lon();
- loc_lat = loc->get_lat();
- nav_x = loc->get_x();
- nav_y = loc->get_y();
- nav_z = loc->get_z();
- last_nav_id = nav_id;
- last_nav_vor = false;
- loc_node->setBoolValue( true );
- has_dme = (dme != NULL);
- if ( gs != NULL ) {
- has_gs_node->setBoolValue( true );
- gs_lon = gs->get_lon();
- gs_lat = gs->get_lat();
- nav_elev = gs->get_elev_ft();
- int tmp = (int)(gs->get_multiuse() / 1000.0);
- target_gs = (double)tmp / 100.0;
- gs_x = gs->get_x();
- gs_y = gs->get_y();
- gs_z = gs->get_z();
-
- // derive GS baseline (perpendicular to the runay
- // along the ground)
- double tlon, tlat, taz;
- geo_direct_wgs_84 ( 0.0, gs_lat, gs_lon,
- target_radial + 90,
- 100.0, &tlat, &tlon, &taz );
- // cout << "target_radial = " << target_radial << endl;
- // cout << "nav_loc = " << loc_node->getBoolValue() << endl;
- // cout << gs_lon << "," << gs_lat << " "
- // << tlon << "," << tlat << " (" << nav_elev << ")"
- // << endl;
- Point3D p1 = sgGeodToCart( Point3D(tlon*SGD_DEGREES_TO_RADIANS,
- tlat*SGD_DEGREES_TO_RADIANS,
- nav_elev*SG_FEET_TO_METER)
- );
- // cout << gs_x << "," << gs_y << "," << gs_z
- // << endl;
- // cout << p1 << endl;
- sgdSetVec3( gs_base_vec,
- p1.x()-gs_x, p1.y()-gs_y, p1.z()-gs_z );
- // cout << gs_base_vec[0] << "," << gs_base_vec[1] << ","
- // << gs_base_vec[2] << endl;
- } else {
- has_gs_node->setBoolValue( false );
- nav_elev = loc->get_elev_ft();
- }
- twist = 0;
- range = FG_LOC_DEFAULT_RANGE;
- effective_range = range;
-
- if ( globals->get_soundmgr()->exists( nav_fx_name ) ) {
- globals->get_soundmgr()->remove( nav_fx_name );
- }
- SGSoundSample *sound;
- sound = morse.make_ident( trans_ident, LO_FREQUENCY );
- sound->set_volume( 0.3 );
- globals->get_soundmgr()->add( sound, nav_fx_name );
-
- if ( globals->get_soundmgr()->exists( dme_fx_name ) ) {
- globals->get_soundmgr()->remove( dme_fx_name );
- }
- sound = morse.make_ident( trans_ident, HI_FREQUENCY );
- sound->set_volume( 0.3 );
- globals->get_soundmgr()->add( sound, dme_fx_name );
-
- int offset = (int)(sg_random() * 30.0);
- play_count = offset / 4;
- last_time = globals->get_time_params()->get_cur_time() -
- offset;
- // cout << "offset = " << offset << " play_count = "
- // << play_count
- // << " last_time = " << last_time
- // << " current time = "
- // << globals->get_time_params()->get_cur_time() << endl;
-
- // cout << "Found an loc station in range" << endl;
- // cout << " id = " << loc->get_locident() << endl;
- }
- } else if ( nav != NULL ) {
- nav_id = nav->get_ident();
- nav_id_node->setStringValue( nav_id.c_str() );
- // cout << "nav = " << nav_id << endl;
- is_valid = true;
- if ( last_nav_id != nav_id || !last_nav_vor ) {
- last_nav_id = nav_id;
- last_nav_vor = true;
- trans_ident = nav->get_trans_ident();
- loc_node->setBoolValue( false );
- has_dme = (dme != NULL);
- has_gs_node->setBoolValue( false );
- loc_lon = nav->get_lon();
- loc_lat = nav->get_lat();
- nav_elev = nav->get_elev_ft();
- twist = nav->get_multiuse();
- range = nav->get_range();
- effective_range = adjustNavRange(nav_elev, elev, range);
- target_gs = 0.0;
- target_radial = sel_radial_node->getDoubleValue();
- nav_x = nav->get_x();
- nav_y = nav->get_y();
- nav_z = nav->get_z();
-
- if ( globals->get_soundmgr()->exists( nav_fx_name ) ) {
- globals->get_soundmgr()->remove( nav_fx_name );
- }
- try {
- SGSoundSample *sound;
- sound = morse.make_ident( trans_ident, LO_FREQUENCY );
- sound->set_volume( 0.3 );
- if ( globals->get_soundmgr()->add( sound, nav_fx_name ) ) {
- // cout << "Added nav-vor-ident sound" << endl;
- } else {
- SG_LOG(SG_COCKPIT, SG_WARN, "Failed to add v1-vor-ident sound");
- }
-
- if ( globals->get_soundmgr()->exists( dme_fx_name ) ) {
- globals->get_soundmgr()->remove( dme_fx_name );
- }
- sound = morse.make_ident( trans_ident, HI_FREQUENCY );
- sound->set_volume( 0.3 );
- globals->get_soundmgr()->add( sound, dme_fx_name );
-
- int offset = (int)(sg_random() * 30.0);
- play_count = offset / 4;
- last_time = globals->get_time_params()->get_cur_time() - offset;
- // cout << "offset = " << offset << " play_count = "
- // << play_count << " last_time = "
- // << last_time << " current time = "
- // << globals->get_time_params()->get_cur_time() << endl;
-
- // cout << "Found a vor station in range" << endl;
- // cout << " id = " << nav->get_ident() << endl;
- } catch ( sg_io_exception &e ) {
- SG_LOG(SG_GENERAL, SG_ALERT, e.getFormattedMessage());
- }
- }
- } else {
- is_valid = false;
- nav_id_node->setStringValue( "" );
- target_radial = 0;
- trans_ident = "";
- last_nav_id = "";
- if ( ! globals->get_soundmgr()->remove( nav_fx_name ) ) {
- SG_LOG(SG_COCKPIT, SG_WARN, "Failed to remove nav-vor-ident sound");
- }
- globals->get_soundmgr()->remove( dme_fx_name );
- // cout << "not picking up vor1. :-(" << endl;
+void FGNavRadio::audioNavidChanged()
+{
+ if ( globals->get_soundmgr()->exists(nav_fx_name)) {
+ globals->get_soundmgr()->remove(nav_fx_name);
+ }
+
+ try {
+ string trans_ident(_navaid->get_trans_ident());
+ SGSoundSample* sound = morse.make_ident(trans_ident, LO_FREQUENCY);
+ sound->set_volume( 0.3 );
+ if (!globals->get_soundmgr()->add( sound, nav_fx_name )) {
+ SG_LOG(SG_COCKPIT, SG_WARN, "Failed to add v1-vor-ident sound");
}
- is_valid_node->setBoolValue( is_valid );
-
- char tmpid[5];
- strncpy( tmpid, nav_id.c_str(), 5 );
- id_c1_node->setIntValue( (int)tmpid[0] );
- id_c2_node->setIntValue( (int)tmpid[1] );
- id_c3_node->setIntValue( (int)tmpid[2] );
- id_c4_node->setIntValue( (int)tmpid[3] );
+ if ( globals->get_soundmgr()->exists( dme_fx_name ) ) {
+ globals->get_soundmgr()->remove( dme_fx_name );
+ }
+
+ sound = morse.make_ident( trans_ident, HI_FREQUENCY );
+ sound->set_volume( 0.3 );
+ globals->get_soundmgr()->add( sound, dme_fx_name );
+
+ int offset = (int)(sg_random() * 30.0);
+ play_count = offset / 4;
+ last_time = globals->get_time_params()->get_cur_time() - offset;
+ } catch (sg_io_exception& e) {
+ SG_LOG(SG_GENERAL, SG_ALERT, e.getFormattedMessage());
+ }
}
projects / flightgear.git / blobdiff