//
// Written by Curtis Olson, started May 1997.
//
-// Copyright (C) 1997 Curtis L. Olson - curt@infoplane.com
+// Copyright (C) 1997 Curtis L. Olson - http://www.flightgear.org/~curt
//
// This program is free software; you can redistribute it and/or
// modify it under the terms of the GNU General Public License as
#include <simgear/constants.h>
#include <simgear/debug/logstream.hxx>
#include <simgear/math/sg_geodesy.hxx>
+#include <simgear/scene/model/placement.hxx>
#include <simgear/timing/timestamp.hxx>
#include <Scenery/scenery.hxx>
-#include <FDM/LaRCsim/ls_interface.h>
#include <Main/globals.hxx>
#include <Main/fg_props.hxx>
+#include <FDM/groundcache.hxx>
-#include "External.hxx"
#include "flight.hxx"
-#include "JSBSim.hxx"
-#include "LaRCsim.hxx"
-#include "Balloon.h"
// base_fdm_state is the internal state that is updated in integer
}
// Constructor
-FGInterface::FGInterface() {
+FGInterface::FGInterface()
+ : remainder(0)
+{
_setup();
}
-FGInterface::FGInterface( double dt ) {
+FGInterface::FGInterface( double dt )
+ : remainder(0)
+{
_setup();
- delta_t = dt;
- remainder = elapsed = multi_loop = 0;
}
// Destructor
}
+int
+FGInterface::_calc_multiloop (double dt)
+{
+ int hz = fgGetInt("/sim/model-hz");
+ int speedup = fgGetInt("/sim/speed-up");
+
+ dt += remainder;
+ remainder = 0;
+ double ml = dt * hz;
+ // Avoid roundoff problems by adding the roundoff itself.
+ // ... ok, two times the roundoff to have enough room.
+ int multiloop = int(floor(ml * (1.0 + 2.0*DBL_EPSILON)));
+ remainder = (ml - multiloop) / hz;
+ return (multiloop * speedup);
+}
+
+
/**
* Set default values for the state of the FDM.
*
set_inited( true );
- stamp();
- set_remainder( 0 );
+// stamp();
+// set_remainder( 0 );
// Set initial position
SG_LOG( SG_FLIGHT, SG_INFO, "...initializing position..." );
- set_Longitude( fgGetDouble("/position/longitude-deg")
+ set_Longitude( fgGetDouble("/sim/presets/longitude-deg")
* SGD_DEGREES_TO_RADIANS );
- set_Latitude( fgGetDouble("/position/latitude-deg")
+ set_Latitude( fgGetDouble("/sim/presets/latitude-deg")
* SGD_DEGREES_TO_RADIANS );
- double ground_elev_m = scenery.get_cur_elev();
+ double ground_elev_m = globals->get_scenery()->get_cur_elev();
double ground_elev_ft = ground_elev_m * SG_METER_TO_FEET;
- if ( fgGetBool("/sim/startup/onground")
- || fgGetDouble("/position/altitude-ft") < ground_elev_ft ) {
+ fgSetDouble("/position/ground-elev-m", ground_elev_m);
+ _set_Runway_altitude ( ground_elev_ft );
+ if ( fgGetBool("/sim/presets/onground")
+ || fgGetDouble("/sim/presets/altitude-ft") < ground_elev_ft ) {
fgSetDouble("/position/altitude-ft", ground_elev_ft);
+ set_Altitude( ground_elev_ft );
+ } else {
+ set_Altitude( fgGetDouble("/sim/presets/altitude-ft") );
}
- set_Altitude( fgGetDouble("/position/altitude-ft") );
// Set ground elevation
SG_LOG( SG_FLIGHT, SG_INFO,
// Set sea-level radius
SG_LOG( SG_FLIGHT, SG_INFO, "...initializing sea-level radius..." );
SG_LOG( SG_FLIGHT, SG_INFO, " lat = "
- << fgGetDouble("/position/latitude-deg")
- << " alt = " << fgGetDouble("/position/altitude-ft") );
+ << fgGetDouble("/sim/presets/latitude-deg")
+ << " alt = " << get_Altitude() );
double sea_level_radius_meters;
double lat_geoc;
- sgGeodToGeoc( fgGetDouble("/position/latitude-deg")
+ sgGeodToGeoc( fgGetDouble("/sim/presets/latitude-deg")
* SGD_DEGREES_TO_RADIANS,
- fgGetDouble("/position/altitude-ft") * SG_FEET_TO_METER,
+ get_Altitude() * SG_FEET_TO_METER,
&sea_level_radius_meters, &lat_geoc );
_set_Sea_level_radius( sea_level_radius_meters * SG_METER_TO_FEET );
// Set initial velocities
SG_LOG( SG_FLIGHT, SG_INFO, "...initializing velocities..." );
- if ( !fgHasNode("/sim/startup/speed-set") ) {
+ if ( !fgHasNode("/sim/presets/speed-set") ) {
set_V_calibrated_kts(0.0);
} else {
- const string speedset = fgGetString("/sim/startup/speed-set");
+ const string speedset = fgGetString("/sim/presets/speed-set");
if ( speedset == "knots" || speedset == "KNOTS" ) {
- set_V_calibrated_kts( fgGetDouble("/velocities/airspeed-kt") );
+ set_V_calibrated_kts( fgGetDouble("/sim/presets/airspeed-kt") );
} else if ( speedset == "mach" || speedset == "MACH" ) {
- set_Mach_number( fgGetDouble("/velocities/mach") );
+ set_Mach_number( fgGetDouble("/sim/presets/mach") );
} else if ( speedset == "UVW" || speedset == "uvw" ) {
set_Velocities_Wind_Body(
- fgGetDouble("/velocities/uBody-fps"),
- fgGetDouble("/velocities/vBody-fps"),
- fgGetDouble("/velocities/wBody-fps") );
+ fgGetDouble("/sim/presets/uBody-fps"),
+ fgGetDouble("/sim/presets/vBody-fps"),
+ fgGetDouble("/sim/presets/wBody-fps") );
} else if ( speedset == "NED" || speedset == "ned" ) {
set_Velocities_Local(
- fgGetDouble("/velocities/speed-north-fps"),
- fgGetDouble("/velocities/speed-east-fps"),
- fgGetDouble("/velocities/speed-down-fps") );
+ fgGetDouble("/sim/presets/speed-north-fps"),
+ fgGetDouble("/sim/presets/speed-east-fps"),
+ fgGetDouble("/sim/presets/speed-down-fps") );
} else {
SG_LOG( SG_FLIGHT, SG_ALERT,
- "Unrecognized value for /sim/startup/speed-set: "
+ "Unrecognized value for /sim/presets/speed-set: "
<< speedset);
set_V_calibrated_kts( 0.0 );
}
// Set initial Euler angles
SG_LOG( SG_FLIGHT, SG_INFO, "...initializing Euler angles..." );
- set_Euler_Angles( fgGetDouble("/orientation/roll-deg")
+ set_Euler_Angles( fgGetDouble("/sim/presets/roll-deg")
* SGD_DEGREES_TO_RADIANS,
- fgGetDouble("/orientation/pitch-deg")
+ fgGetDouble("/sim/presets/pitch-deg")
* SGD_DEGREES_TO_RADIANS,
- fgGetDouble("/orientation/heading-deg")
+ fgGetDouble("/sim/presets/heading-deg")
* SGD_DEGREES_TO_RADIANS );
SG_LOG( SG_FLIGHT, SG_INFO, "End common FDM init" );
bound = true;
// Time management (read-only)
- fgTie("/fdm/time/delta_t", this,
- &FGInterface::get_delta_t); // read-only
- fgTie("/fdm/time/elapsed", this,
- &FGInterface::get_elapsed); // read-only
- fgTie("/fdm/time/remainder", this,
- &FGInterface::get_remainder); // read-only
- fgTie("/fdm/time/multi_loop", this,
- &FGInterface::get_multi_loop); // read-only
+// fgTie("/fdm/time/delta_t", this,
+// &FGInterface::get_delta_t); // read-only
+// fgTie("/fdm/time/elapsed", this,
+// &FGInterface::get_elapsed); // read-only
+// fgTie("/fdm/time/remainder", this,
+// &FGInterface::get_remainder); // read-only
+// fgTie("/fdm/time/multi_loop", this,
+// &FGInterface::get_multi_loop); // read-only
// Aircraft position
fgTie("/position/latitude-deg", this,
&FGInterface::set_Psi_deg);
fgSetArchivable("/orientation/heading-deg");
+ // Body-axis "euler rates" (rotation speed, but in a funny
+ // representation).
+ fgTie("/orientation/roll-rate-degps", this,
+ &FGInterface::get_Phi_dot_degps);
+ fgTie("/orientation/pitch-rate-degps", this,
+ &FGInterface::get_Theta_dot_degps);
+ fgTie("/orientation/yaw-rate-degps", this,
+ &FGInterface::get_Psi_dot_degps);
+
// Calibrated airspeed
fgTie("/velocities/airspeed-kt", this,
&FGInterface::get_V_calibrated_kts,
&FGInterface::set_V_calibrated_kts,
+ false);
+
+ // Mach number
+ fgTie("/velocities/mach", this,
+ &FGInterface::get_Mach_number,
+ &FGInterface::set_Mach_number,
false);
// Local velocities
fgTie("/velocities/glideslope", this,
&FGInterface::get_Gamma_vert_rad,
&FGInterface::set_Gamma_vert_rad );
- fgTie("/velocities/side-slip-rad", this,
+ fgTie("/orientation/side-slip-rad", this,
&FGInterface::get_Beta); // read-only
- fgTie("/velocities/side-slip-deg", this,
+ fgTie("/orientation/side-slip-deg", this,
&FGInterface::get_Beta_deg); // read-only
- fgTie("/velocities/alpha-deg", this,
+ fgTie("/orientation/alpha-deg", this,
&FGInterface::get_Alpha_deg); // read-only
fgTie("/accelerations/nlf", this,
&FGInterface::get_Nlf); // read-only
+
+ // NED accelerations
+ fgTie("/accelerations/ned/north-accel-fps_sec",
+ this, &FGInterface::get_V_dot_north);
+ fgTie("/accelerations/ned/east-accel-fps_sec",
+ this, &FGInterface::get_V_dot_east);
+ fgTie("/accelerations/ned/down-accel-fps_sec",
+ this, &FGInterface::get_V_dot_down);
+
+ // Pilot accelerations
+ fgTie("/accelerations/pilot/x-accel-fps_sec",
+ this, &FGInterface::get_A_X_pilot);
+ fgTie("/accelerations/pilot/y-accel-fps_sec",
+ this, &FGInterface::get_A_Y_pilot);
+ fgTie("/accelerations/pilot/z-accel-fps_sec",
+ this, &FGInterface::get_A_Z_pilot);
+
}
{
bound = false;
- fgUntie("/fdm/time/delta_t");
- fgUntie("/fdm/time/elapsed");
- fgUntie("/fdm/time/remainder");
- fgUntie("/fdm/time/multi_loop");
+ // fgUntie("/fdm/time/delta_t");
+ // fgUntie("/fdm/time/elapsed");
+ // fgUntie("/fdm/time/remainder");
+ // fgUntie("/fdm/time/multi_loop");
fgUntie("/position/latitude-deg");
fgUntie("/position/longitude-deg");
fgUntie("/position/altitude-ft");
fgUntie("/position/altitude-agl-ft");
- fgUntie("/orientation/heading-deg");
- fgUntie("/orientation/pitch-deg");
fgUntie("/orientation/roll-deg");
+ fgUntie("/orientation/pitch-deg");
+ fgUntie("/orientation/heading-deg");
+ fgUntie("/orientation/roll-rate-degps");
+ fgUntie("/orientation/pitch-rate-degps");
+ fgUntie("/orientation/yaw-rate-degps");
+ fgUntie("/orientation/side-slip-rad");
+ fgUntie("/orientation/side-slip-deg");
+ fgUntie("/orientation/alpha-deg");
fgUntie("/velocities/airspeed-kt");
+ fgUntie("/velocities/mach");
fgUntie("/velocities/speed-north-fps");
fgUntie("/velocities/speed-east-fps");
fgUntie("/velocities/speed-down-fps");
fgUntie("/velocities/wBody-fps");
fgUntie("/velocities/vertical-speed-fps");
fgUntie("/velocities/glideslope");
- fgUntie("/velocities/side-slip-rad");
- fgUntie("/velocities/side-slip-deg");
- fgUntie("/velocities/alpha-deg");
fgUntie("/accelerations/nlf");
-
+ fgUntie("/accelerations/pilot/x-accel-fps_sec");
+ fgUntie("/accelerations/pilot/y-accel-fps_sec");
+ fgUntie("/accelerations/pilot/z-accel-fps_sec");
+ fgUntie("/accelerations/ned/north-accel-fps_sec");
+ fgUntie("/accelerations/ned/east-accel-fps_sec");
+ fgUntie("/accelerations/ned/down-accel-fps_sec");
}
/**
* Update the state of the FDM (i.e. run the equations of motion).
*/
void
-FGInterface::update (int dt)
+FGInterface::update (double dt)
{
- cout << "dummy update() ... SHOULDN'T BE CALLED!" << endl;
+ SG_LOG(SG_FLIGHT, SG_ALERT, "dummy update() ... SHOULDN'T BE CALLED!");
}
_set_Geodetic_Position( lat, lon, alt );
_set_Sea_level_radius( sl_radius * SG_METER_TO_FEET );
- _set_Runway_altitude( scenery.get_cur_elev() * SG_METER_TO_FEET );
+ _set_Runway_altitude( fgGetDouble("/position/ground-elev-m") * SG_METER_TO_FEET );
_set_sin_lat_geocentric( lat_geoc );
_set_cos_lat_geocentric( lat_geoc );
_set_Geodetic_Position( lat_geod, lon, alt );
_set_Sea_level_radius( sl_radius2 * SG_METER_TO_FEET );
- _set_Runway_altitude( scenery.get_cur_elev() * SG_METER_TO_FEET );
+ _set_Runway_altitude( fgGetDouble("/position/ground-elev-m") * SG_METER_TO_FEET );
_set_sin_lat_geocentric( lat_geoc );
_set_cos_lat_geocentric( lat_geoc );
// -dw- metrowerks complains about ambiguous access, not critical
// to keep this ;)
#ifndef __MWERKS__
- cout << "extrapolating FDM by dt = " << dt << endl;
+ SG_LOG(SG_FLIGHT, SG_INFO, "extrapolating FDM by dt = " << dt);
#endif
double lat = geodetic_position_v[0] + geocentric_rates_v[0] * dt;
SG_LOG(SG_FLIGHT,SG_INFO,"altitude_agl: " << altitude_agl );
}
+bool
+FGInterface::prepare_ground_cache_m(double ref_time, const double pt[3],
+ double rad)
+{
+ return ground_cache.prepare_ground_cache(ref_time, pt, rad);
+}
+
+bool FGInterface::prepare_ground_cache_ft(double ref_time, const double pt[3],
+ double rad)
+{
+ // Convert units and do the real work.
+ sgdVec3 pt_ft;
+ sgdScaleVec3( pt_ft, pt, SG_FEET_TO_METER );
+ return ground_cache.prepare_ground_cache(ref_time, pt_ft, rad*SG_FEET_TO_METER);
+}
+
+bool
+FGInterface::is_valid_m(double *ref_time, double pt[3], double *rad)
+{
+ return ground_cache.is_valid(ref_time, pt, rad);
+}
+
+bool FGInterface::is_valid_ft(double *ref_time, double pt[3], double *rad)
+{
+ // Convert units and do the real work.
+ bool found_ground = ground_cache.is_valid(ref_time, pt, rad);
+ sgdScaleVec3(pt, SG_METER_TO_FEET);
+ *rad *= SG_METER_TO_FEET;
+ return found_ground;
+}
+
+double
+FGInterface::get_cat_m(double t, const double pt[3],
+ double end[2][3], double vel[2][3])
+{
+ return ground_cache.get_cat(t, pt, end, vel);
+}
+
+double
+FGInterface::get_cat_ft(double t, const double pt[3],
+ double end[2][3], double vel[2][3])
+{
+ // Convert units and do the real work.
+ sgdVec3 pt_m;
+ sgdScaleVec3( pt_m, pt, SG_FEET_TO_METER );
+ double dist = ground_cache.get_cat(t, pt_m, end, vel);
+ for (int k=0; k<2; ++k) {
+ sgdScaleVec3( end[k], SG_METER_TO_FEET );
+ sgdScaleVec3( vel[k], SG_METER_TO_FEET );
+ }
+ return dist*SG_METER_TO_FEET;
+}
+
+bool
+FGInterface::get_agl_m(double t, const double pt[3],
+ double contact[3], double normal[3], double vel[3],
+ int *type, double *loadCapacity,
+ double *frictionFactor, double *agl)
+{
+ return ground_cache.get_agl(t, pt, contact, normal, vel, type,
+ loadCapacity, frictionFactor, agl);
+}
+
+bool
+FGInterface::get_agl_ft(double t, const double pt[3],
+ double contact[3], double normal[3], double vel[3],
+ int *type, double *loadCapacity,
+ double *frictionFactor, double *agl)
+{
+ // Convert units and do the real work.
+ sgdVec3 pt_m;
+ sgdScaleVec3( pt_m, pt, SG_FEET_TO_METER );
+ bool ret = ground_cache.get_agl(t, pt_m, contact, normal, vel,
+ type, loadCapacity, frictionFactor, agl);
+ // Convert units back ...
+ sgdScaleVec3( contact, SG_METER_TO_FEET );
+ sgdScaleVec3( vel, SG_METER_TO_FEET );
+ *agl *= SG_METER_TO_FEET;
+ // FIXME: scale the load limit to something in the english unit system.
+ // Be careful with the DBL_MAX which is returned by default.
+ return ret;
+}
+
+bool
+FGInterface::caught_wire_m(double t, const double pt[4][3])
+{
+ return ground_cache.caught_wire(t, pt);
+}
+
+bool
+FGInterface::caught_wire_ft(double t, const double pt[4][3])
+{
+ // Convert units and do the real work.
+ double pt_m[4][3];
+ for (int i=0; i<4; ++i)
+ sgdScaleVec3(pt_m[i], pt[i], SG_FEET_TO_METER);
+
+ return ground_cache.caught_wire(t, pt_m);
+}
+
+bool
+FGInterface::get_wire_ends_m(double t, double end[2][3], double vel[2][3])
+{
+ return ground_cache.get_wire_ends(t, end, vel);
+}
+
+bool
+FGInterface::get_wire_ends_ft(double t, double end[2][3], double vel[2][3])
+{
+ // Convert units and do the real work.
+ bool ret = ground_cache.get_wire_ends(t, end, vel);
+ for (int k=0; k<2; ++k) {
+ sgdScaleVec3( end[k], SG_METER_TO_FEET );
+ sgdScaleVec3( vel[k], SG_METER_TO_FEET );
+ }
+ return ret;
+}
+
+void
+FGInterface::release_wire(void)
+{
+ ground_cache.release_wire();
+}
void fgToggleFDMdataLogging(void) {
cur_fdm_state->ToggleDataLogging();