A robust gain-scheduled controller is designed for the longitudinal attitude control of a light commercial aircraft using an Hinfinity approach. Following a model reduction procedure that exploits the optimal controller structure, linear time-invariant controllers designed at the selected equilibrium points are reduced to second order controllers and realized in a feedback path configuration that is amenable to scheduling. A gain-scheduling law is developed and simulation results verify that the closed-loop performance specifications are met.


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    Titel :

    Robust gain-scheduled aircraft longitudinal controller design using an Hinfinity approach


    Beteiligte:
    Lin, Z. (Autor:in) / Khammash, M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2001


    Format / Umfang :

    6 Seiten, 10 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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