A device including an acquisition module for acquiring current parameters of the aircraft, a computational module for computing a current load factor of the aircraft, a computational module for computing a minimum load factor, a computational module for computing the difference between the current load factor and the minimum load factor, and an acoustic emission module for emitting a sound signal, the level of which increases gradually as a function of time when the difference between the current load factor and the minimum load factor is less than zero.
Method and device for assisting with the landing of an aircraft during a flare maneuver
2019-04-30
Patent
Electronic Resource
English
European Patent Office | 2018
|European Patent Office | 2017
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