The command generator tracker (CGT) technique is used to design an explicit model following scheme in which the stabilizing feedback control law is designed to be a redundant control law. The scheme is applicable to the self-repairing flight control system concept. The A-7D DIGITAC aircraft linearized data, at one flight condition and one type of impairment, is employed to demonstrate the validaty of the approach. The employment of a redundant control law will increase the survivability and operational reliability of the aircraft and will enhance its maintainability during the combat and peace time missions.


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    Title :

    Redundant command generator tracker control technique for self-repairing flight control systems


    Additional title:

    Ein redundantes Nachlaufsteuerungsverfahren fuer Fuehrungsgeneratoren fuer sich selbst reparierende Flugregelungssysteme


    Contributors:
    Sadeghi, T. (author)


    Publication date :

    1984


    Size :

    3 Seiten, 7 Bilder, 2 Tabellen, 8 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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