| 摘要 |
The invention relates to a rotorcraft cockpit having a left seat and a right seat placed side-by-side, a console extending between the seats, two side sticks, one situated to the right of the right seat and the other situated to the left of the left seat, enabling the pilot to control roll and pitch; a flight control system comprising sensors associated with the side sticks and a computer connected to the sensors serves to convert the orders applied by the pilot to the side sticks into signals for controlling actuators in order to vary roll and pitch; a piloting relationship integrated in the computer stabilizes the response of the rotorcraft in roll and in pitch when a side stick is actuated, and maintains the attitudes in roll and pitch at reference values when neither side stick is actuated.
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