| 摘要 |
<p>A method and apparatus for controlling a flight of an aircraft. An undesired change in an airspeed for the aircraft is identified. A number of commands for a flight control system associated with a wing of the aircraft are identified in response to the undesired change in the airspeed. The number of commands is configured to cause the flight control system to maintain a lift of the aircraft for a desired trajectory.</p> |
