DocumentCode
3072243
Title
Application of system identification to aircraft flight test data processing
Author
Anderson, L.C. ; Vincent, J.H.
Author_Institution
Systems Control Techonology Inc., Palo Alto, California
fYear
1985
fDate
11-13 Dec. 1985
Firstpage
1929
Lastpage
1931
Abstract
A nonlinear aerodynamic model for the AV-8B aircraft in the post-stall and departure region was identified from flight test data. A Principal Components Regression algorithm was used to identify model parameters. The identification methodology is described, and the results are compared with wind tunnel derived models.
Keywords
Aerodynamics; Aerospace control; Aerospace electronics; Aerospace simulation; Aircraft; Computer graphics; Control systems; Data processing; System identification; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1985 24th IEEE Conference on
Conference_Location
Fort Lauderdale, FL, USA
Type
conf
DOI
10.1109/CDC.1985.268918
Filename
4048656
Link To Document