Progress made during the quarter Jan. to Apr. 1989 on research into a modified stepwise regression method for estimating the stability and control derivatives of a British Aerospace Hawk aircraft, from data obtained by use of a scaled model on a dynamic wind tunnel test rig, is discussed. The objectives are described and the program status is reported as running on schedule. Future objectives are outlined.
Application of Modified Stepwise Regression for the Estimation of Aircraft Stability and Control Parameters
1989
48 pages
Report
Keine Angabe
Englisch