| 摘要 |
Disclosed are a control device, a control system, and a control method of an aircraft. The control device comprises a first control rod. The movement of the first control rod in a first movement direction controls the motion of the aircraft in a first motion direction, and after the external force applied on the first control rod in the first movement direction is removed, the first control rod automatically returns to a predetermined position in the first movement direction. When the first control rod automatically returns to the predetermined position, the aircraft maintains a flying state in the first motion direction, and the flying state is maintained depending on a control signal received by the aircraft that is generated when the external force applied on the first control rod in the first motion direction changes and a state signal that is measured by a state measurement sensor carried by the aircraft. |
