A series of flight tests were conducted on the PC 9/A aircraft, A23- 045, at the Royal Australian Air Force's Aircraft Research and Development Unit. System identification techniques were applied to the data obtained from these flight tests to determine the stability and control derivatives of the aircraft. The lateral results for the aircraft in cruise configuration are presented in this report and comparisons are made with empirical and ground based estimates.


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    Title :

    Correlation between Flight-determined Lateral Derivatives and Ground- based Data for the Pilatus PC 9/A Training Aircraft in Cruise Configuration


    Contributors:

    Publication date :

    2000


    Size :

    59 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English