| 摘要 |
<p>The invention relates to a control device for aircraft comprising at least one aircraft undercarriage 4a, 4b, 4c arranged on an aircraft 1, which aircraft undercarriage has one or more undercarriage wheels 3, and comprising a control mechanism 5 which interacts with the aircraft undercarriage 4a, 4b, 4c and which is set up to turn the undercarriage wheels 3 relative to the longitudinal axis A of the aircraft 1. The control device has an alignment unit 6 which is connected to the control mechanism 5 and which is set up to control the turning of the undercarriage wheels 3 by means of the control mechanism 5 during at least one part of the landing or take-off phase I, II, III of the aircraft 1, in such a way that the running direction of the undercarriage wheels 3 is aligned in the direction of a fixed point 9, which may be a corrected fixed point situated below a fixed point 9 by a compensation angle.</p> |
