METHOD FOR SIMULATING FLIGHT ATTITUDES OF AN AIRCRAFT CAPABLE OF VERTICAL TAKEOFF AND/OR VERTICAL LANDING

摘要

In a method for simulating flight attitudes of an aircraft capable of vertical take-off and/or vertical landing, with a simulator having a movement device configured as an industrial robot having serial kinematics, wherein movements of a first support for at least one subject positioned on the movement device are controlled by at least one control element, it is proposed for a realistic simulation of critical flight attitudes that the at least one control element is actuated by a subject positioned in the first support such that a ground contact device connected to the first support, such as skids and/or a landing gear, is lifted off a ground or set down on a ground.