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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    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    1981


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch