Rotor aircraft e.g. civilian helicopter, changes movement state of main portion in deflection direction during deflection of operating element, and represents dynamics of main portion by feedback forces acting on control element

摘要

The rotor aircraft (1) has a control element (3) for generating the control commands (6) to drive and steering unit (7) of the main portion. The control element is provided with an operating element (4) which is deflected relative to the main portion movably defined in an initial position. The control element is adapted to change the movement state of the main portion in the deflection direction, during a deflection of operating element. The change of the deflection is dependent. The dynamics of the main portion are represented by the feedback forces acting on the control element.