In one embodiment, a flight control system is configured to receive one or more pilot inputs intended to effect a particular control outcome for the aircraft, receive one or more current flight parameters of the aircraft, determine whether or not the aircraft is near or in a stall, and if it is determined that the aircraft is near or in a stall, automatically control the aircraft's flight control surfaces in an oscillatory manner that increases the sensitivity of the flight control surfaces and achieves the pilot's intended control outcome.


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    Title :

    Systems And Methods For Controlling An Aircraft's Flight Control Surfaces


    Contributors:
    HASSAN AHMED (author) / TAHA HAITHEM (author)

    Publication date :

    2020-07-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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