FIELD: aviation.
SUBSTANCE: flight control device for aerial vehicle (1) comprises a support (2), a lever (3) rotatably mounted on the support, and a mechanical means for creating a return force for the lever. The specified device includes the spring (6) and the first motor element (13) located so that the first end of the spring is forced to move rotationally by the lever, and the other end of the spring is forced to move rotationally by the output shaft the first motor element. The flight control device includes an electric assist system (18) for facilitating the said mechanical means in generating a return force comprising a second motor element and a control means for the second motor element.
EFFECT: easier change in the return force acting on the control lever is provided.
13 cl, 7 dwg
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