An aircraft includes a ground maneuver control system that automatically steers a nose landing gear wheel to compensate for asymmetrical braking of the wheels of the aircraft resulting from a failure on one side in comparison to the other. A control system detects such a failure in order to be able to effect such automatic steering. The system may be retrofitted by the installation of software on an existing aircraft, having a braking and steering computer system with a pre-existing steering control functional block and a pre-existing braking control functional block.
SYSTEM FOR CONTROLLING AIRCRAFT GROUND MANOEUVRES
25.07.2024
Patent
Elektronische Ressource
Englisch
METHOD AND APPARATUS FOR CONTROLLING AIRCRAFT GROUND MANOEUVRES
Europäisches Patentamt | 2024
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