Failure detection and identification logic for a fault-tolerant longitudinal control system were investigated. Aircraft dynamics were based upon the cruise condition for a hypothetical transonic business jet transport configuration. The fault-tolerant control system consists of conventional control and estimation plus a new outer loop containing failure detection, identification, and reconfiguration (FDIR) logic. It is assumed that the additional logic has access to all measurements, as well as to the outputs of the control and estimation logic. The pilot may also command the FDIR logic to perform special tests.


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    Title :

    Failure Detection and Identification for a Reconfigurable Flight Control System


    Contributors:
    F. Dallery (author)

    Publication date :

    1987


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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