Objective: Obtain models for unsteady aerodynamics of fixed-wing MAVs (e.g. incorporating dynamic stall, vortex shedding). Technical approach: Systematic models using approximate balanced truncation (balanced POD); empirical, phenomenological models that capture correct bifurcation behavior.


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    Titel :

    Unsteady Aerodynamic Models for Flight Control of Agile Micro Air Vehicles


    Beteiligte:
    C. Rowley (Autor:in)

    Erscheinungsdatum :

    2008


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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