The accuracy of aircraft stability and control derivatives as estimated from dynamic response measurements depends on the form of the time histories of the control inputs. After selecting a suitable criterion and imposing constraints on either the aircraft's state or the control inputs it is possible to optimize the form of these time histories. A method for control input optimization is proposed which avoids some disadvantages of earlier methods and was successfully applied in the design of longitudinal and lateral flight test maneuvers.


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    Titel :

    Optimal Inputs for Aircraft Parameter Estimation


    Beteiligte:
    J. A. Mulder (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    36 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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