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
1979-04-01
Report
Keine Angabe
Englisch
An Aircraft Structural Integrity Program - FAA Flight Inspection Beech 300 Fleet
British Library Conference Proceedings | 1995
|Beech Aircraft Reliability Program
SAE Technical Papers | 1965
|