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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    Title :

    Unsteady Aerodynamic Models for Flight Control of Agile Micro Air Vehicles


    Contributors:
    C. Rowley (author)

    Publication date :

    2008


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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