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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    Titel :

    Aircraft flight test trajectory control


    Beteiligte:
    Menon, P. K. A. (Autor:in) / Walker, R. A. (Autor:in)

    Erscheinungsdatum :

    1988-01-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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