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Issue 1090: Adapt the mk-viii instrument code to the new internal runway scheme.

Clean up some unneeded functions as well and make use of standard simgear functions where possible.
This whole thing could need a rewrite...
This commit is contained in:
Christian Schmitt 2013-03-27 20:02:07 +01:00
parent 913727239d
commit db5a39e305
2 changed files with 39 additions and 231 deletions

View file

@ -66,8 +66,13 @@
#include <simgear/constants.h> #include <simgear/constants.h>
#include <simgear/sg_inlines.h> #include <simgear/sg_inlines.h>
#include <simgear/debug/logstream.hxx> #include <simgear/debug/logstream.hxx>
#include <simgear/math/sg_geodesy.hxx> #include <simgear/math/SGMathFwd.hxx>
#include <simgear/math/SGLimits.hxx>
#include <simgear/math/SGGeometryFwd.hxx>
#include <simgear/math/SGGeodesy.hxx>
#include <simgear/math/sg_random.h> #include <simgear/math/sg_random.h>
#include <simgear/math/SGLineSegment.hxx>
#include <simgear/math/SGIntersect.hxx>
#include <simgear/misc/sg_path.hxx> #include <simgear/misc/sg_path.hxx>
#include <simgear/sound/soundmgr_openal.hxx> #include <simgear/sound/soundmgr_openal.hxx>
#include <simgear/sound/sample_group.hxx> #include <simgear/sound/sample_group.hxx>
@ -136,24 +141,6 @@ modify_amplitude (double amplitude, double dB)
return amplitude * pow(10.0, dB / 20.0); return amplitude * pow(10.0, dB / 20.0);
} }
static double
heading_add (double h1, double h2)
{
double result = h1 + h2;
if (result >= 360)
result -= 360;
return result;
}
static double
heading_substract (double h1, double h2)
{
double result = h1 - h2;
if (result < 0)
result += 360;
return result;
}
static double static double
get_heading_difference (double h1, double h2) get_heading_difference (double h1, double h2)
{ {
@ -167,12 +154,6 @@ get_heading_difference (double h1, double h2)
return fabs(diff); return fabs(diff);
} }
static double
get_reciprocal_heading (double h)
{
return heading_add(h, 180);
}
/////////////////////////////////////////////////////////////////////////////// ///////////////////////////////////////////////////////////////////////////////
// PropertiesHandler ////////////////////////////////////////////////////////// // PropertiesHandler //////////////////////////////////////////////////////////
/////////////////////////////////////////////////////////////////////////////// ///////////////////////////////////////////////////////////////////////////////
@ -4068,9 +4049,7 @@ MK_VIII::Mode6Handler::test_runway (const FGRunway *_runway)
SGGeod::fromDeg(mk_data(gps_longitude).get(), mk_data(gps_latitude).get())); SGGeod::fromDeg(mk_data(gps_longitude).get(), mk_data(gps_latitude).get()));
// get distance to threshold // get distance to threshold
double distance, az1, az2; return SGGeodesy::distanceNm(pos, _runway->threshold()) <= 5;
SGGeodesy::inverse(pos, _runway->threshold(), az1, az2, distance);
return distance * SG_METER_TO_NM <= 5;
} }
bool bool
@ -4270,60 +4249,6 @@ MK_VIII::Mode6Handler::update ()
// TCFHandler ///////////////////////////////////////////////////////////////// // TCFHandler /////////////////////////////////////////////////////////////////
/////////////////////////////////////////////////////////////////////////////// ///////////////////////////////////////////////////////////////////////////////
// Gets the difference between the azimuth from @from_lat,@from_lon to
// @to_lat,@to_lon, and @to_heading, in degrees.
double
MK_VIII::TCFHandler::get_azimuth_difference (double from_lat,
double from_lon,
double to_lat,
double to_lon,
double to_heading)
{
double az1, az2, distance;
geo_inverse_wgs_84(0, from_lat, from_lon, to_lat, to_lon, &az1, &az2, &distance);
return get_heading_difference(az1, to_heading);
}
// Gets the difference between the azimuth from the current GPS
// position to the center of @_runway, and the heading of @_runway, in
// degrees.
double
MK_VIII::TCFHandler::get_azimuth_difference (const FGRunway *_runway)
{
return get_azimuth_difference(mk_data(gps_latitude).get(),
mk_data(gps_longitude).get(),
_runway->latitude(),
_runway->longitude(),
_runway->headingDeg());
}
// Selects the most likely intended destination runway of @airport,
// and returns it in @_runway. For each runway, the difference between
// the azimuth from the current GPS position to the center of the
// runway and its heading is computed. The runway having the smallest
// difference wins.
//
// This selection algorithm is not specified in [SPEC], but
// http://www.egpws.com/general_information/description/runway_select.htm
// talks about automatic runway selection.
FGRunway*
MK_VIII::TCFHandler::select_runway (const FGAirport *airport)
{
FGRunway* _runway = 0;
double min_diff = 360;
for (unsigned int r=0; r<airport->numRunways(); ++r) {
FGRunway* rwy(airport->getRunwayByIndex(r));
double diff = get_azimuth_difference(rwy);
if (diff < min_diff)
{
min_diff = diff;
_runway = rwy;
}
} // of airport runways iteration
return _runway;
}
bool MK_VIII::TCFHandler::AirportFilter::passAirport(FGAirport* aApt) const bool MK_VIII::TCFHandler::AirportFilter::passAirport(FGAirport* aApt) const
{ {
return aApt->hasHardRunwayOfLengthFt(mk->conf.runway_database); return aApt->hasHardRunwayOfLengthFt(mk->conf.runway_database);
@ -4343,109 +4268,43 @@ MK_VIII::TCFHandler::update_runway ()
// large airports, which may have a runway located far away from // large airports, which may have a runway located far away from
// the airport's reference point. // the airport's reference point.
AirportFilter filter(mk); AirportFilter filter(mk);
FGAirport* apt = FGAirport::findClosest( SGGeod apos = SGGeod::fromDeg(mk_data(gps_longitude).get(), mk_data(gps_latitude).get());
SGGeod::fromDeg(mk_data(gps_longitude).get(), mk_data(gps_latitude).get()), FGAirport* apt = FGAirport::findClosest(apos, 30.0, &filter);
30.0, &filter);
if (!apt) return; if (!apt) return;
FGRunway* _runway = select_runway(apt); FGRunway* _runway = apt->findBestRunwayForPos(apos).get();
if (!_runway) return; if (!_runway) return;
has_runway = true; has_runway = true;
runway.center.latitude = _runway->latitude(); runway.center = _runway->pointOnCenterline(_runway->lengthM() * 0.5);
runway.center.longitude = _runway->longitude();
runway.elevation = apt->elevation(); runway.elevation = apt->elevation();
runway.half_width_m = _runway->widthM() * 0.5;
double half_length_m = _runway->lengthM() * 0.5; double half_length_m = _runway->lengthM() * 0.5;
runway.half_length = half_length_m * SG_METER_TO_NM; runway.half_length = half_length_m * SG_METER_TO_NM;
// b3 ________________ b0 // ________________
// | | // | |
// h1>>> | e1<<<<<<<<e0 | <<<h0 // h1>>> | e1<<<<<<<<e0 | <<<h0
// |________________| // |________________|
// b2 b1
// get heading to runway threshold (h0) and end (h1) // get heading to runway threshold (h0) and end (h1)
runway.edges[0].heading = _runway->headingDeg(); runway.edges[0].heading = _runway->headingDeg();
runway.edges[1].heading = get_reciprocal_heading(_runway->headingDeg()); runway.edges[1].heading = _runway->reciprocalRunway()->headingDeg();
double az;
// get position of runway threshold (e0) // get position of runway threshold (e0)
geo_direct_wgs_84(0, runway.edges[0].position = _runway->begin();
runway.center.latitude,
runway.center.longitude,
runway.edges[1].heading,
half_length_m,
&runway.edges[0].position.latitude,
&runway.edges[0].position.longitude,
&az);
// get position of runway end (e1) // get position of runway end (e1)
geo_direct_wgs_84(0, runway.edges[1].position = _runway->end();
runway.center.latitude,
runway.center.longitude,
runway.edges[0].heading,
half_length_m,
&runway.edges[1].position.latitude,
&runway.edges[1].position.longitude,
&az);
double half_width_m = _runway->widthM() * 0.5; // get cartesian coordinates of both runway ends
runway.bias_points[0] = _runway->cart();
// get position of threshold bias area edges (b0 and b1) runway.bias_points[1] = _runway->reciprocalRunway()->cart();
get_bias_area_edges(&runway.edges[0].position,
runway.edges[1].heading,
half_width_m,
&runway.bias_area[0],
&runway.bias_area[1]);
// get position of end bias area edges (b2 and b3)
get_bias_area_edges(&runway.edges[1].position,
runway.edges[0].heading,
half_width_m,
&runway.bias_area[2],
&runway.bias_area[3]);
}
void
MK_VIII::TCFHandler::get_bias_area_edges (Position *edge,
double reciprocal,
double half_width_m,
Position *bias_edge1,
Position *bias_edge2)
{
double half_bias_width_m = k * SG_NM_TO_METER + half_width_m;
double tmp_latitude = 0.0, tmp_longitude = 0.0, az = 0.0;
geo_direct_wgs_84(0,
edge->latitude,
edge->longitude,
reciprocal,
k * SG_NM_TO_METER,
&tmp_latitude,
&tmp_longitude,
&az);
geo_direct_wgs_84(0,
tmp_latitude,
tmp_longitude,
heading_substract(reciprocal, 90),
half_bias_width_m,
&bias_edge1->latitude,
&bias_edge1->longitude,
&az);
geo_direct_wgs_84(0,
tmp_latitude,
tmp_longitude,
heading_add(reciprocal, 90),
half_bias_width_m,
&bias_edge2->latitude,
&bias_edge2->longitude,
&az);
} }
// Returns true if the current GPS position is inside the edge // Returns true if the current GPS position is inside the edge
@ -4457,11 +4316,10 @@ MK_VIII::TCFHandler::get_bias_area_edges (Position *edge,
bool bool
MK_VIII::TCFHandler::is_inside_edge_triangle (RunwayEdge *edge) MK_VIII::TCFHandler::is_inside_edge_triangle (RunwayEdge *edge)
{ {
return get_azimuth_difference(mk_data(gps_latitude).get(), double az = SGGeodesy::courseDeg( SGGeod::fromDeg(mk_data(gps_longitude).get(),
mk_data(gps_longitude).get(), mk_data(gps_latitude).get()),
edge->position.latitude, edge->position);
edge->position.longitude, return get_heading_difference(az, edge->heading) <= 45;
edge->heading) <= 45;
} }
// Returns true if the current GPS position is inside the bias area of // Returns true if the current GPS position is inside the bias area of
@ -4469,30 +4327,10 @@ MK_VIII::TCFHandler::is_inside_edge_triangle (RunwayEdge *edge)
bool bool
MK_VIII::TCFHandler::is_inside_bias_area () MK_VIII::TCFHandler::is_inside_bias_area ()
{ {
double az1[4]; double half_bias_width_m = k * SG_NM_TO_METER + runway.half_width_m;
double angles_sum = 0; SGVec3d cpos = SGVec3d::fromGeod( SGGeod::fromDeg(mk_data(gps_longitude).get(), mk_data(gps_latitude).get()) );
SGLineSegmentd bias_line = SGLineSegmentd(runway.bias_points[0], runway.bias_points[1]);
for (int i = 0; i < 4; i++) return dist(cpos, bias_line) < half_bias_width_m;
{
double az2, distance;
geo_inverse_wgs_84(0,
mk_data(gps_latitude).get(),
mk_data(gps_longitude).get(),
runway.bias_area[i].latitude,
runway.bias_area[i].longitude,
&az1[i], &az2, &distance);
}
for (int i = 0; i < 4; i++)
{
double angle = az1[i == 3 ? 0 : i + 1] - az1[i];
if (angle < -180)
angle += 360;
angles_sum += angle;
}
return angles_sum > 180;
} }
bool bool
@ -4502,17 +4340,9 @@ MK_VIII::TCFHandler::is_tcf ()
{ {
if (has_runway) if (has_runway)
{ {
double distance, az1, az2; double distance = SGGeodesy::distanceNm( SGGeod::fromDeg(mk_data(gps_longitude).get(),
mk_data(gps_latitude).get()),
geo_inverse_wgs_84(0, runway.center);
mk_data(gps_latitude).get(),
mk_data(gps_longitude).get(),
runway.center.latitude,
runway.center.longitude,
&az1, &az2, &distance);
distance *= SG_METER_TO_NM;
// distance to the inner envelope edge // distance to the inner envelope edge
double edge_distance = distance - runway.half_length - k; double edge_distance = distance - runway.half_length - k;
@ -4576,16 +4406,13 @@ MK_VIII::TCFHandler::is_rfcf ()
{ {
if (has_runway) if (has_runway)
{ {
double distance, az1, az2;
geo_inverse_wgs_84(0, double distance = SGGeodesy::distanceNm( SGGeod::fromDeg(mk_data(gps_longitude).get(),
mk_data(gps_latitude).get(), mk_data(gps_latitude).get()),
mk_data(gps_longitude).get(), runway.center);
runway.center.latitude,
runway.center.longitude,
&az1, &az2, &distance);
double krf = k + mk_data(gps_vertical_figure_of_merit).get() / 200; double krf = k + mk_data(gps_vertical_figure_of_merit).get() / 200;
distance = distance * SG_METER_TO_NM - runway.half_length - krf; distance = distance - runway.half_length - krf;
if (distance <= 5) if (distance <= 5)
{ {

View file

@ -1270,13 +1270,7 @@ private:
{ {
typedef struct typedef struct
{ {
double latitude; // latitude in degrees SGGeod position; // position of threshold
double longitude; // longitude in degrees
} Position;
typedef struct
{
Position position; // position of threshold
double heading; // runway heading double heading; // runway heading
} RunwayEdge; } RunwayEdge;
@ -1289,33 +1283,20 @@ private:
struct struct
{ {
Position center; // center point SGGeod center; // center point
double elevation; // elevation in feet double elevation; // elevation in feet
double half_length; // runway half length, in nautical miles double half_length; // runway half length, in nautical miles
double half_width_m; // runway half width, in meters
RunwayEdge edges[2]; // runway threshold and end RunwayEdge edges[2]; // runway threshold and end
Position bias_area[4]; // vertices of the bias area SGVec3d bias_points[2]; // vertices of the bias area
} runway; } runway;
double bias; double bias;
double *reference; double *reference;
double initial_value; double initial_value;
double get_azimuth_difference (double from_lat,
double from_lon,
double to_lat,
double to_lon,
double to_heading);
double get_azimuth_difference (const FGRunway *_runway);
FGRunway* select_runway (const FGAirport *airport);
void update_runway (); void update_runway ();
void get_bias_area_edges (Position *edge,
double reciprocal,
double half_width_m,
Position *bias_edge1,
Position *bias_edge2);
bool is_inside_edge_triangle (RunwayEdge *edge); bool is_inside_edge_triangle (RunwayEdge *edge);
bool is_inside_bias_area (); bool is_inside_bias_area ();