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.


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    Title :

    Application of system identification to aircraft flight test data processing


    Additional title:

    Anwendung der Systemidentifikation auf die Verarbeitung von Flugtestdaten


    Contributors:


    Publication date :

    1985


    Size :

    3 Seiten, 6 Bilder, 3 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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