Two design techniques for linear flight test trajectory controllers (FTTCs) are described: Eigenstructure assignment and the minimum error excitation technique. The two techniques are used to design FTTCs for an F-15 aircraft model for eight different maneuvers at thirty different flight conditions. An evaluation of the FTTCs is presented.


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    Title :

    Aircraft flight test trajectory control


    Contributors:

    Publication date :

    1988-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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