inline void set_TargetDistance( double val ) { TargetDistance = val; }
inline double get_TargetAltitude() const { return TargetAltitude; }
inline void set_TargetAltitude( double val ) { TargetAltitude = val; }
+ inline double get_TargetAGL() const { return TargetAGL; }
+ inline void set_TargetAGL( double val ) { TargetAGL = val; }
inline double get_TargetClimbRate() const { return TargetClimbRate; }
inline void set_TargetClimbRate( double val ) { TargetClimbRate = val; }
_set_Geodetic_Position( Latitude, tmp_lon, Altitude );
_set_Euler_Angles( Phi, Theta, Psi );
- _set_Altitude_AGL( Altitude-Runway_altitude );
+ _set_Altitude_AGL( Altitude - Runway_altitude );
// Miscellaneous quantities
_set_T_Local_to_Body(T_local_to_body_m);
{
current_autopilot->set_AltitudeMode(FGAutopilot::FG_ALTITUDE_TERRAIN);
current_autopilot->set_AltitudeEnabled(lock);
+ current_autopilot->set_TargetAGL(
+ current_aircraft.fdm_state->get_Altitude_AGL() * SG_FEET_TO_METER
+ );
+ cout << "Target AGL = "
+ << current_aircraft.fdm_state->get_Altitude_AGL() * SG_FEET_TO_METER
+ << endl;
}
fgSetArchivable("/autopilot/locks/glide-slope");
fgTie("/autopilot/locks/terrain", getAPTerrainLock, setAPTerrainLock);
fgSetArchivable("/autopilot/locks/terrain");
+ fgTie("/autopilot/settings/agl-ft", getAPAltitude, setAPAltitude);
+ fgSetArchivable("/autopilot/settings/agl-ft");
fgTie("/autopilot/settings/climb-rate-fpm", getAPClimb, setAPClimb, false);
fgSetArchivable("/autopilot/settings/climb-rate-fpm");
fgTie("/autopilot/locks/heading", getAPHeadingLock, setAPHeadingLock);
FGAndCondition::~FGAndCondition ()
{
- for (int i = 0; i < _conditions.size(); i++)
+ for (unsigned int i = 0; i < _conditions.size(); i++)
delete _conditions[i];
}
FGOrCondition::~FGOrCondition ()
{
- for (int i = 0; i < _conditions.size(); i++)
+ for (unsigned int i = 0; i < _conditions.size(); i++)
delete _conditions[i];
}