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.
Stability and Control Derivative Estimates Obtained from Flight Data for the Beech 99 Aircraft
1979
38 pages
Report
No indication
English
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