speed_up = fgGetNode("/sim/speed-up", true);
aero = fgGetNode("/sim/aero", true);
-
+
ls_toplevel_init( 0.0, (char *)(aero->getStringValue().c_str()) );
lsic=new LaRCsimIC; //this needs to be brought up after LaRCsim is
if ( aero->getStringValue() == "c172" ) {
- copy_to_LaRCsim(); // initialize all of LaRCsim's vars
-
- //this should go away someday -- formerly done in fg_init.cxx
- Mass = 8.547270E+01;
- I_xx = 1.048000E+03;
- I_yy = 3.000000E+03;
- I_zz = 3.530000E+03;
- I_xz = 0.000000E+00;
+ copy_to_LaRCsim(); // initialize all of LaRCsim's vars
+
+ //this should go away someday -- formerly done in fg_init.cxx
+ Mass = 8.547270E+01;
+ I_xx = 1.048000E+03;
+ I_yy = 3.000000E+03;
+ I_zz = 3.530000E+03;
+ I_xz = 0.000000E+00;
}
-
+
ls_set_model_dt( get_delta_t() );
-
- // Initialize our little engine that hopefully might
+
+ // Initialize our little engine that hopefully might
eng.init( get_delta_t() );
// dcl - in passing dt to init rather than update I am assuming
// that the LaRCsim dt is fixed at one value (yes it is 120hz CLO)
// Also note that this is the max quantity - the usable quantity
// is slightly less
set_Tank1Fuel(28.0);
- set_Tank2Fuel(28.0);
+ set_Tank2Fuel(28.0);
}
FGLaRCsim::~FGLaRCsim(void) {
if ( lsic != NULL ) {
- delete lsic;
- lsic = NULL;
+ free_engines();
+ delete lsic;
+ lsic = NULL;
}
-}
+}
// Initialize the LaRCsim flight model, dt is the time increment for
// each subsequent iteration through the EOM
// copy control positions into the LaRCsim structure
Lat_control = globals->get_controls()->get_aileron() /
- speed_up->getIntValue();
+ speed_up->getIntValue();
Long_control = globals->get_controls()->get_elevator();
Long_trim = globals->get_controls()->get_elevator_trim();
Rudder_pedal = globals->get_controls()->get_rudder() /
Flap_handle = 30.0 * globals->get_controls()->get_flaps();
if ( aero->getStringValue() == "c172" ) {
- Use_External_Engine = 1;
+ Use_External_Engine = 1;
} else {
Use_External_Engine = 0;
}
SG_LOG( SG_FLIGHT, SG_INFO, " V_north_airmass: " << V_north_airmass );
SG_LOG( SG_FLIGHT, SG_INFO, " V_east_airmass: " << V_east_airmass );
SG_LOG( SG_FLIGHT, SG_INFO, " V_down_airmass: " << V_down_airmass );
-}
+}
void FGLaRCsim::snap_shot(void) {
lsic->SetLatitudeGDRadIC( get_Latitude() );
lsic->SetLatitudeGDRadIC(lat);
set_ls();
copy_from_LaRCsim(); //update the bus
-}
+}
void FGLaRCsim::set_Longitude(double lon) {
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Longitude: " << lon );
lsic->SetLongitudeRadIC(lon);
set_ls();
copy_from_LaRCsim(); //update the bus
-}
+}
void FGLaRCsim::set_Altitude(double alt) {
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Altitude: " << alt );
lsic->SetVcalibratedKtsIC(vc);
set_ls();
copy_from_LaRCsim(); //update the bus
-}
+}
void FGLaRCsim::set_Mach_number(double mach) {
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Mach_number: " << mach );
lsic->SetMachIC(mach);
set_ls();
copy_from_LaRCsim(); //update the bus
-}
+}
void FGLaRCsim::set_Velocities_Local( double north, double east, double down ){
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Velocities_local: "
lsic->SetVNEDFpsIC(north, east, down);
set_ls();
copy_from_LaRCsim(); //update the bus
-}
+}
void FGLaRCsim::set_Velocities_Wind_Body( double u, double v, double w){
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Velocities_Wind_Body: "
lsic->SetUVWFpsIC(u,v,w);
set_ls();
copy_from_LaRCsim(); //update the bus
-}
+}
//Euler angles
void FGLaRCsim::set_Euler_Angles( double phi, double theta, double psi ) {
lsic->SetRollAngleRadIC(phi);
lsic->SetHeadingRadIC(psi);
set_ls();
- copy_from_LaRCsim(); //update the bus
-}
+ copy_from_LaRCsim(); //update the bus
+}
//Flight Path
void FGLaRCsim::set_Climb_Rate( double roc) {
snap_shot();
lsic->SetClimbRateFpsIC(roc);
set_ls();
- copy_from_LaRCsim(); //update the bus
-}
+ copy_from_LaRCsim(); //update the bus
+}
void FGLaRCsim::set_Gamma_vert_rad( double gamma) {
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Gamma_vert_rad: " << gamma );
snap_shot();
lsic->SetFlightPathAngleRadIC(gamma);
set_ls();
- copy_from_LaRCsim(); //update the bus
-}
+ copy_from_LaRCsim(); //update the bus
+}
void FGLaRCsim::set_Runway_altitude(double ralt) {
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Runway_altitude: " << ralt );
snap_shot();
lsic->SetRunwayAltitudeFtIC(ralt);
set_ls();
- copy_from_LaRCsim(); //update the bus
-}
+ copy_from_LaRCsim(); //update the bus
+}
void FGLaRCsim::set_AltitudeAGL(double altagl) {
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_AltitudeAGL: " << altagl );
lsic->SetVNEDAirmassFpsIC( wnorth, weast, wdown );
set_ls();
copy_from_LaRCsim();
-}
+}
void FGLaRCsim::set_Static_pressure(double p) {
SG_LOG( SG_FLIGHT, SG_INFO,
}
-void FGLaRCsim::set_Density(double rho) {
+void FGLaRCsim::set_Density(double rho) {
SG_LOG( SG_FLIGHT, SG_INFO, "FGLaRCsim::set_Density: " << rho );
SG_LOG( SG_FLIGHT, SG_INFO,
"LaRCsim does not support externally supplied atmospheric data" );
inline void init_vec(FG_VECTOR_3 vec) {
vec[0] = 0.0; vec[1] = 0.0; vec[2] = 0.0;
-}
+}
FGEngInterface::FGEngInterface() {
-
+
// inputs
Throttle=0;
Mixture=0;
x=y=z=0.0;
brake=rolls=WoW=false;
position=1.0;
-}
+}
FGGearInterface::~FGGearInterface() {
}
// Constructor
FGInterface::FGInterface() {
_setup();
-}
+}
FGInterface::FGInterface( double dt ) {
_setup();
// Destructor
FGInterface::~FGInterface() {
-// unbind(); // FIXME: should be called explicitly
+ // unbind(); // FIXME: should be called explicitly
}
init_vec( n_pilot_body_v );
init_vec( omega_dot_body_v );
init_vec( v_local_v );
- init_vec( v_local_rel_ground_v );
- init_vec( v_local_airmass_v );
- init_vec( v_local_rel_airmass_v );
- init_vec( v_local_gust_v );
- init_vec( v_wind_body_v );
- init_vec( omega_body_v );
- init_vec( omega_local_v );
- init_vec( omega_total_v );
+ init_vec( v_local_rel_ground_v );
+ init_vec( v_local_airmass_v );
+ init_vec( v_local_rel_airmass_v );
+ init_vec( v_local_gust_v );
+ init_vec( v_wind_body_v );
+ init_vec( omega_body_v );
+ init_vec( omega_local_v );
+ init_vec( omega_total_v );
init_vec( euler_rates_v );
- init_vec( geocentric_rates_v );
+ init_vec( geocentric_rates_v );
init_vec( geocentric_position_v );
init_vec( geodetic_position_v );
init_vec( euler_angles_v );
- init_vec( d_cg_rwy_local_v );
- init_vec( d_cg_rwy_rwy_v );
- init_vec( d_pilot_rwy_local_v );
- init_vec( d_pilot_rwy_rwy_v );
+ init_vec( d_cg_rwy_local_v );
+ init_vec( d_cg_rwy_rwy_v );
+ init_vec( d_pilot_rwy_local_v );
+ init_vec( d_pilot_rwy_rwy_v );
init_vec( t_local_to_body_m[0] );
init_vec( t_local_to_body_m[1] );
init_vec( t_local_to_body_m[2] );
-
+
mass=i_xx=i_yy=i_zz=i_xz=0;
- nlf=0;
+ nlf=0;
v_rel_wind=v_true_kts=v_rel_ground=v_inertial=0;
v_ground_speed=v_equiv=v_equiv_kts=0;
v_calibrated=v_calibrated_kts=0;
- gravity=0;
- centrifugal_relief=0;
- alpha=beta=alpha_dot=beta_dot=0;
+ gravity=0;
+ centrifugal_relief=0;
+ alpha=beta=alpha_dot=beta_dot=0;
cos_alpha=sin_alpha=cos_beta=sin_beta=0;
cos_phi=sin_phi=cos_theta=sin_theta=cos_psi=sin_psi=0;
- gamma_vert_rad=gamma_horiz_rad=0;
+ gamma_vert_rad=gamma_horiz_rad=0;
sigma=density=v_sound=mach_number=0;
static_pressure=total_pressure=impact_pressure=0;
dynamic_pressure=0;
runway_altitude=runway_latitude=runway_longitude=0;
runway_heading=0;
radius_to_rwy=0;
- climb_rate=0;
+ climb_rate=0;
sin_lat_geocentric=cos_lat_geocentric=0;
sin_latitude=cos_latitude=0;
sin_longitude=cos_longitude=0;
*
* Subclasses of FGInterface may do their own, additional initialization,
* but there is some that is common to all. Normally, they should call
- * this before they begin their own init to make sure the basic structures
+ * this before they begin their own init to make sure the basic structures
* are set up properly.
*/
void
"...initializing ground elevation to " << ground_elev_ft
<< "ft..." );
SG_LOG( SG_FLIGHT, SG_INFO, "common_init(): set ground elevation "
- << ground_elev_ft );
+ << ground_elev_ft );
base_fdm_state.set_Runway_altitude( ground_elev_ft );
set_Runway_altitude( ground_elev_ft );
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::get_Latitude_deg,
- &FGInterface::set_Latitude_deg,
- false);
+ &FGInterface::get_Latitude_deg,
+ &FGInterface::set_Latitude_deg,
+ false);
fgSetArchivable("/position/latitude-deg");
fgTie("/position/longitude-deg", this,
- &FGInterface::get_Longitude_deg,
- &FGInterface::set_Longitude_deg,
- false);
+ &FGInterface::get_Longitude_deg,
+ &FGInterface::set_Longitude_deg,
+ false);
fgSetArchivable("/position/longitude-deg");
fgTie("/position/altitude-ft", this,
- &FGInterface::get_Altitude,
- &FGInterface::set_Altitude,
- false);
+ &FGInterface::get_Altitude,
+ &FGInterface::set_Altitude,
+ false);
fgSetArchivable("/position/altitude-ft");
fgTie("/position/altitude-agl-ft", this,
- &FGInterface::get_Altitude_AGL); // read-only
+ &FGInterface::get_Altitude_AGL); // read-only
// Orientation
fgTie("/orientation/roll-deg", this,
}
}
+void
+FGInterface::free_engines ()
+{
+ int i;
+ for ( i = 0; i < get_num_engines(); ++i ) {
+ delete get_engine(i);
+ }
+ engines.clear();
+}
+
+void
+FGInterface::free_gear_units ()
+{
+ int i;
+ for ( i = 0; i < get_num_gear(); ++i ) {
+ delete [] get_gear_unit(i);
+ }
+ gear.clear();
+}
/**
* Update the state of the FDM (i.e. run the equations of motion).
return false;
}
-
+
void FGInterface::_updatePosition( double lat_geoc, double lon, double alt ) {
double lat_geod, tmp_alt, sl_radius1, sl_radius2, tmp_lat_geoc;
-
+
// cout << "starting sea level rad = " << get_Sea_level_radius() << endl;
sgGeocToGeod( lat_geoc, ( get_Sea_level_radius() + alt ) * SG_FEET_TO_METER,
sl_radius2 * SG_METER_TO_FEET + alt );
_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( scenery.get_cur_elev() * SG_METER_TO_FEET );
+
_set_sin_lat_geocentric( lat_geoc );
_set_cos_lat_geocentric( lat_geoc );
-
+
_set_sin_cos_longitude( lon );
-
+
_set_sin_cos_latitude( lat_geod );
-
+
/* Norman's code for slope of the terrain */
/* needs to be tested -- get it on the HUD and taxi around */
/* double *tnorm = scenery.cur_normal;
-
+
double sy = sin ( -get_Psi() ) ;
double cy = cos ( -get_Psi() ) ;
double phitb, thetatb, psitb;
- if(tnorm[1] != 0.0) {
- psitb = -atan2 ( tnorm[0], tnorm[1] );
+ if ( tnorm[1] != 0.0 ) {
+ psitb = -atan2 ( tnorm[0], tnorm[1] );
}
- if(tnorm[2] != 0.0) {
- thetatb = atan2 ( tnorm[0] * cy - tnorm[1] * sy, tnorm[2] );
- phitb = -atan2 ( tnorm[1] * cy + tnorm[0] * sy, tnorm[2] );
+ if ( tnorm[2] != 0.0 ) {
+ thetatb = atan2 ( tnorm[0] * cy - tnorm[1] * sy, tnorm[2] );
+ phitb = -atan2 ( tnorm[1] * cy + tnorm[0] * sy, tnorm[2] );
}
_set_terrain_slope(phitb, thetatb, psitb)
// Set the altitude (force)
void fgFDMForceAltitude(const string &model, double alt_meters) {
SG_LOG(SG_FLIGHT,SG_INFO, "fgFDMForceAltitude: " << alt_meters );
-
+
double sea_level_radius_meters;
double lat_geoc;
cur_fdm_state->set_Altitude( alt_meters * SG_METER_TO_FEET );
cur_fdm_state->set_Sea_level_radius( sea_level_radius_meters *
- SG_METER_TO_FEET );
+ SG_METER_TO_FEET );
// additional work needed for some flight models
if ( model == "larcsim" ) {
// Positions
-void FGInterface::set_Latitude(double lat) {
+void FGInterface::set_Latitude(double lat) {
geodetic_position_v[0] = lat;
-}
+}
void FGInterface::set_Longitude(double lon) {
geodetic_position_v[1] = lon;
-}
+}
void FGInterface::set_Altitude(double alt) {
geodetic_position_v[2] = alt;
-}
+}
void FGInterface::set_AltitudeAGL(double altagl) {
altitude_agl=altagl;
-}
+}
// Velocities
void FGInterface::set_V_calibrated_kts(double vc) {
v_calibrated_kts = vc;
-}
+}
void FGInterface::set_Mach_number(double mach) {
mach_number = mach;
-}
+}
void FGInterface::set_Velocities_Local( double north,
double east,
double down ){
v_local_v[0] = north;
v_local_v[1] = east;
- v_local_v[2] = down;
-}
+ v_local_v[2] = down;
+}
void FGInterface::set_Velocities_Wind_Body( double u,
double v,
v_wind_body_v[0] = u;
v_wind_body_v[1] = v;
v_wind_body_v[2] = w;
-}
+}
// Euler angles
void FGInterface::set_Euler_Angles( double phi,
// Flight Path
void FGInterface::set_Climb_Rate( double roc) {
climb_rate = roc;
-}
+}
void FGInterface::set_Gamma_vert_rad( double gamma) {
gamma_vert_rad = gamma;
-}
+}
// Earth
void FGInterface::set_Sea_level_radius(double slr) {
sea_level_radius = slr;
-}
+}
void FGInterface::set_Runway_altitude(double ralt) {
runway_altitude = ralt;
-}
+}
void FGInterface::set_Static_pressure(double p) { static_pressure = p; }
void FGInterface::set_Static_temperature(double T) { static_temperature = T; }
v_local_airmass_v[0] = wnorth;
v_local_airmass_v[1] = weast;
v_local_airmass_v[2] = wdown;
-}
+}
void FGInterface::_busdump(void) {
SG_LOG(SG_FLIGHT,SG_INFO,"d_cg_rwy_rwy_v[3]: " << d_cg_rwy_rwy_v[0] << ", " << d_cg_rwy_rwy_v[1] << ", " << d_cg_rwy_rwy_v[2]);
SG_LOG(SG_FLIGHT,SG_INFO,"d_pilot_rwy_local_v[3]: " << d_pilot_rwy_local_v[0] << ", " << d_pilot_rwy_local_v[1] << ", " << d_pilot_rwy_local_v[2]);
SG_LOG(SG_FLIGHT,SG_INFO,"d_pilot_rwy_rwy_v[3]: " << d_pilot_rwy_rwy_v[0] << ", " << d_pilot_rwy_rwy_v[1] << ", " << d_pilot_rwy_rwy_v[2]);
-
+
SG_LOG(SG_FLIGHT,SG_INFO,"t_local_to_body_m[0][3]: " << t_local_to_body_m[0][0] << ", " << t_local_to_body_m[0][1] << ", " << t_local_to_body_m[0][2]);
SG_LOG(SG_FLIGHT,SG_INFO,"t_local_to_body_m[1][3]: " << t_local_to_body_m[1][0] << ", " << t_local_to_body_m[1][1] << ", " << t_local_to_body_m[1][2]);
SG_LOG(SG_FLIGHT,SG_INFO,"t_local_to_body_m[2][3]: " << t_local_to_body_m[2][0] << ", " << t_local_to_body_m[2][1] << ", " << t_local_to_body_m[2][2]);
SG_LOG(SG_FLIGHT,SG_INFO,"sin_latitude: " << sin_latitude );
SG_LOG(SG_FLIGHT,SG_INFO,"cos_latitude: " << cos_latitude );
SG_LOG(SG_FLIGHT,SG_INFO,"altitude_agl: " << altitude_agl );
-}
+}
void fgToggleFDMdataLogging(void) {
<< AptId );
if ( airports.search( AptId, &a ) )
- {
- // unbind the current fdm state so property changes
- // don't get lost when we subsequently delete this fdm
- // and create a new one.
- cur_fdm_state->unbind();
-
- AptId = a.id.c_str(); /// NHV fix wrong case crash
- fgSetString("/sim/startup/airport-id", AptId.c_str() );
- // fgSetDouble("/position/altitude-ft", -9999.0 );
- // fgSetPosFromAirportID( AptId );
- fgSetPosFromAirportIDandHdg( AptId,
- cur_fdm_state->get_Psi() *
- SGD_RADIANS_TO_DEGREES);
- BusyCursor(0);
- fgReInitSubsystems();
- // if ( global_tile_mgr.init() ) {
- // Load the local scenery data
- global_tile_mgr.update( longitude->getDoubleValue(),
- latitude->getDoubleValue() );
- // } else {
- // SG_LOG( SG_GENERAL, SG_ALERT,
- // "Error in Tile Manager initialization!" );
- // exit(-1);
- // }
- BusyCursor(1);
- } else {
- AptId += " not in database.";
- mkDialog(AptId.c_str());
- }
+ {
+ // unbind the current fdm state so property changes
+ // don't get lost when we subsequently delete this fdm
+ // and create a new one.
+ cur_fdm_state->unbind();
+
+ AptId = a.id.c_str(); /// NHV fix wrong case crash
+ fgSetString("/sim/startup/airport-id", AptId.c_str() );
+ // fgSetDouble("/position/altitude-ft", -9999.0 );
+ // fgSetPosFromAirportID( AptId );
+ fgSetPosFromAirportIDandHdg( AptId,
+ cur_fdm_state->get_Psi() *
+ SGD_RADIANS_TO_DEGREES);
+ BusyCursor(0);
+ fgReInitSubsystems();
+ // if ( global_tile_mgr.init() ) {
+ // Load the local scenery data
+ global_tile_mgr.update( longitude->getDoubleValue(),
+ latitude->getDoubleValue() );
+ // } else {
+ // SG_LOG( SG_GENERAL, SG_ALERT,
+ // "Error in Tile Manager initialization!" );
+ // exit(-1);
+ // }
+ BusyCursor(1);
+ } else {
+ AptId += " not in database.";
+ mkDialog(AptId.c_str());
+ }
}
if ( !freeze ) {
globals->set_freeze( false );
{
// strncpy( NewAirportId, fgGetString("/sim/startup/airport-id").c_str(), 16 );
sprintf( NewAirportId, "%s", fgGetString("/sim/startup/airport-id").c_str() );
- // cout << "NewAirport " << NewAirportId << endl;
+ // cout << "NewAirport " << NewAirportId << endl;
AptDialogInput->setValue( NewAirportId );
FG_PUSH_PUI_DIALOG( AptDialog );
# include <windows.h>
#endif
-#include <GL/glut.h> // needed before pu.h
-#include <plib/pu.h> // plib include
+#include <GL/glut.h> // needed before pu.h
+#include <plib/pu.h> // plib include
+
+#include <FDM/flight.hxx>
#include <Main/globals.hxx>
#include <Main/fg_init.hxx>
#include <Main/fg_props.hxx>
+#include <Scenery/tilemgr.hxx>
+#include <Time/light.hxx>
#include "gui.h"
#include "trackball.h"
float GuiQuat_mat[4][4];
void Quat0( void ) {
- curGuiQuat[0] = _quat0[0];
- curGuiQuat[1] = _quat0[1];
- curGuiQuat[2] = _quat0[2];
- curGuiQuat[3] = _quat0[3];
+ curGuiQuat[0] = _quat0[0];
+ curGuiQuat[1] = _quat0[1];
+ curGuiQuat[2] = _quat0[2];
+ curGuiQuat[3] = _quat0[3];
}
void initMouseQuat(void) {
- trackball(_quat0, 0.0, 0.0, 0.0, 0.0);
- Quat0();
- build_rotmatrix(GuiQuat_mat, curGuiQuat);
+ trackball(_quat0, 0.0, 0.0, 0.0, 0.0);
+ Quat0();
+ build_rotmatrix(GuiQuat_mat, curGuiQuat);
}
void reInit(puObject *cb)
{
- BusyCursor(0);
- Quat0();
-
- // in case user has changed window size as
- // restoreInitialState() overwrites these
- int xsize = fgGetInt("/sim/startup/xsize");
- int ysize = fgGetInt("/sim/startup/ysize");
-
- build_rotmatrix(GuiQuat_mat, curGuiQuat);
- /* check */ globals->restoreInitialState();
-
- fgReInitSubsystems();
-
- fgReshape( xsize, ysize );
-
- BusyCursor(1);
+ BusyCursor(0);
+ Quat0();
+
+ int freeze = globals->get_freeze();
+ if(!freeze)
+ globals->set_freeze( true );
+
+ cur_fdm_state->unbind();
+
+ // in case user has changed window size as
+ // restoreInitialState() overwrites these
+ int xsize = fgGetInt("/sim/startup/xsize");
+ int ysize = fgGetInt("/sim/startup/ysize");
+
+ build_rotmatrix(GuiQuat_mat, curGuiQuat);
+
+ globals->restoreInitialState();
+
+ // Unsuccessful KLUDGE to fix the 'every other time'
+ // problem when doing a 'reset' after a 'goto airport'
+
+ // string AptId( fgGetString("/sim/startup/airport-id") );
+ // if( AptId.c_str() != "\0" )
+ // fgSetPosFromAirportID( AptId );
+
+ fgReInitSubsystems();
+
+ // reduntant(fgReInitSubsystems) ?
+ global_tile_mgr.update( fgGetDouble("/position/longitude-deg"),
+ fgGetDouble("/position/latitude-deg") );
+
+ cur_light_params.Update();
+
+ fgReshape( xsize, ysize );
+
+ BusyCursor(1);
+
+ if ( !freeze ) {
+ globals->set_freeze( false );
+ }
}
projects / flightgear.git / commitdiff