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
2024-07-25
Patent
Electronic Resource
English
METHOD AND APPARATUS FOR CONTROLLING AIRCRAFT GROUND MANOEUVRES
European Patent Office | 2024
|METHOD AND APPARATUS FOR CONTROLLING AIRCRAFT GROUND MANOEUVRES
European Patent Office | 2024
|