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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The Stochastic Control of the F-8C Aircraft Using the Multiple Model Adaptive Control (MMAC) Method


    Contributors:
    M. Athans (author) / K. P. Dunn (author) / C. S. Greene (author) / W. H. Lee (author) / N. R. Sandell (author)

    Publication date :

    1975


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English