NASA-TM-72863
Stability and control derivative estimates obtained from flight data for the Beech 99 aircraft
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Abstract:
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.
Author(s):
R.R. Tanner; T.D. Montgomery
Indexed under:
- None
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