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Controller with control stick for aircraft has 2 control shafts rotatably mounted in fixed position on common frame, joint with free-running device per control shaft for tilting control stick in plane parallel to respective control shaft
Controller with control stick for aircraft has 2 control shafts rotatably mounted in fixed position on common frame, joint with free-running device per control shaft for tilting control stick in plane parallel to respective control shaft
The device has a control stick (7) tiltable about multiple axes for actuating at least two control signal senders for pitch and roll control of the aircraft, two control shafts (3,4) connected to the control stick via a gimbal joint (8) for converting pitch and roll movements of the stick into shaft rotations. The two control shafts are rotatably mounted in a fixed position on a common frame (2) and the joint has a free-running device for each control shaft for tilting of the control stick in a plane parallel to the respective control shaft.
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