This paper describes a technique for flight control system reconfiguration following a control surface failure. The methodology involves the reallocation of flight control commands to the surviving control surfaces following a failure. The algorithms developed are aimed at reconfiguration without pilot intervention and the preservation of normal aircraft flying qualities over an expanded array of fault/battle damage conditions. This ensures that the probability of mission success and completion in the presence of battle damage is increased.


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    Title :

    Self-Repairing Flight Control System


    Additional title:

    Sae Technical Papers


    Contributors:
    McCulloch, B. (author) / Huber, R.R. (author)

    Conference:

    Aerospace Congress and Exposition ; 1984



    Publication date :

    1984-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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