Lateral-directional and longitudinal stability and control derivatives were determined from flight data by using a maximum likelihood estimator for the Beech 99 airplane. Data were obtained with the aircraft in the cruise configuration and with one-third flap deflection. The estimated derivatives show good agreement with the predictions of the manufacturer.


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    Title :

    Stability and Control Derivative Estimates Obtained from Flight Data for the Beech 99 Aircraft


    Contributors:

    Publication date :

    1979


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English