def _compute_propulsion(self, flight_point: FlightPoint): flight_point.thrust = flight_point.drag flight_point.thrust_is_regulated = True self.propulsion.compute_flight_points(flight_point)
def _compute_propulsion(self, flight_point: FlightPoint): flight_point.thrust_rate = self.thrust_rate flight_point.thrust_is_regulated = False self.propulsion.compute_flight_points(flight_point)