The application of a modified stepwise regression algorithm to both a complete data string and to that same data partitioned into bins as a function of angle of attack was demonstrated. Results from the large-scale maneuver agree well with results from 20 maneuvers in which small perturbation from trim at various angles of attack were induced.
Estimation of Airplane Stability and Control Derivatives from Large Amplitude Longitudinal Maneuvers
1981
43 pages
Report
Keine Angabe
Englisch
Airplane longitudinal stability
Engineering Index Backfile | 1937
|Inverse Simulation of Large-Amplitude Aircraft Maneuvers
Online Contents | 1993
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