The application of a modified stepwise regression algorithm to both a complete data string and to that same data partitioned into bins as a function of angle of attack was demonstrated. Results from the large-scale maneuver agree well with results from 20 maneuvers in which small perturbation from trim at various angles of attack were induced.


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    Title :

    Estimation of Airplane Stability and Control Derivatives from Large Amplitude Longitudinal Maneuvers


    Contributors:

    Publication date :

    1981


    Size :

    43 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English