Progress made during the quarter Jan. to Apr. 1989 on research into a modified stepwise regression method for estimating the stability and control derivatives of a British Aerospace Hawk aircraft, from data obtained by use of a scaled model on a dynamic wind tunnel test rig, is discussed. The objectives are described and the program status is reported as running on schedule. Future objectives are outlined.


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    Title :

    Application of Modified Stepwise Regression for the Estimation of Aircraft Stability and Control Parameters


    Contributors:
    H. A. Hinds (author) / M. V. Cook (author)

    Publication date :

    1989


    Size :

    48 pages



    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English