An envelope protection scheme is proposed for responding to a microburst. This approach is based on limiting the allowable maximum inertial deceleration of the aircraft when flying at low airspeeds. This technique is shown in simulations to be very effective at preventing stall and resulting in minimal loss of altitude. It is speculated that the same scheme can also protect an aircraft in the event of other forms of windshear encounters, such as making a sudden turn to downwind.


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    Titel :

    Response of an Advanced Flight Control System to Microburst Encounters


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Singh, B. (Autor:in) / Steck, J. E. (Autor:in) / Rokhsaz, K. (Autor:in) / Chandramohan, R. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 2005



    Erscheinungsdatum :

    2005-10-03




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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