phys_state(self_t &self, phys_aircraft_ptr phys_aircraft, geo_base_3 const& base) : self_(self) //, on_ground_(false) , phys_aircraft_(phys_aircraft) , base_(base) { self.set_nm_angular_smooth(2); self_.set_phys_aircraft(phys_aircraft_); }
phys_state2(self_t &self, aircraft::phys_aircraft_ptr phys_aircraft, geo_base_3 const& base) : self_(self) , desired_speed_(aircraft::min_desired_velocity()) , on_ground_(false) , phys_aircraft_(phys_aircraft) , base_(base) { self.set_nm_angular_smooth(2); self_.set_phys_model(phys_aircraft_); }