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
No indication
English
Stability-Derivative Determination from Flight Data
NTRS | 1958
|Stability-derivative determination from flight data
Engineering Index Backfile | 1960
|