The purpose of this paper is to summarize results obtained for the adaptive control of the F-8C aircraft using the so-called Multiple Model Adaptive Control method. The discussion includes the selection of the performance criteria for both the lateral and the longitudinal dynamics, the design of the Kalman filters for different flight conditions, the 'identification' aspects of the design using hypothesis testing ideas, and the performance of the closed loop adaptive system.


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    Titel :

    The stochastic control of the F-8C aircraft using the Multiple Model Adaptive Control (MMAC) method


    Beteiligte:
    Athans, M. (Autor:in) / Dunn, K. P. (Autor:in) / Greene, E. S. (Autor:in) / Lee, W. H. (Autor:in) / Sandel, N. R., Jr. (Autor:in)

    Kongress:

    IEEE Conf. on Decision and Control 1975 ; 1975 ; Houston, TX, United States


    Erscheinungsdatum :

    01.08.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch