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.
Redundant command generator tracker control technique for self-repairing flight control systems
Ein redundantes Nachlaufsteuerungsverfahren fuer Fuehrungsgeneratoren fuer sich selbst reparierende Flugregelungssysteme
Proc. of the 23rd IEEE Conf. on Decision and Control ; 1 ; 653-655
1984
3 Seiten, 7 Bilder, 2 Tabellen, 8 Quellen
Conference paper
English
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