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.
Application of system identification to aircraft flight test data processing
Anwendung der Systemidentifikation auf die Verarbeitung von Flugtestdaten
Proc. of the 24th IEEE Conf. on Decision and Control ; 3 ; 1929-1931
1985
3 Seiten, 6 Bilder, 3 Quellen
Conference paper
English
Identification of Aircraft Stall Behavior from Flight Test Data
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