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
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;
Conference_Titel :
Decision and Control, 1985 24th IEEE Conference on
Conference_Location :
Fort Lauderdale, FL, USA
DOI :
10.1109/CDC.1985.268918
