The identification of multi-input, single output linear static models from flight test data is discussed. Models based on least squares are considered. Wind tunnel scale model and flight test data on a propeller slipstream are compared. Dynamic flight test data were analyzed by reconstructing the flight path and forming a data base for the identification of aerodynamic models. Given the relatively low Reynolds number of the wind tunnel experiments, a reasonable correspondence exists between the dynamic flight test results and model predictions.


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    Title :

    Aerodynamic Model Identification from Dynamic Flight Test Data and Wind Tunnel Experiments


    Contributors:

    Publication date :

    1982


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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