A design study of adaptive control logic suitable for implementation in modern airborne digital flight computers was conducted. Two designs are described for an example aircraft. Each of these designs uses a weighted least squares procedure to identify parameters defining the dynamics of the aircraft. The two designs differ in the way in which control law parameters are determined. One uses the solution of an optimal linear regulator problem to determine these parameters while the other uses a procedure called single stage optimization. Extensive simulation results and analysis leading to the designs are presented.


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    Title :

    Digital adaptive flight controller development


    Contributors:
    Kaufman, H. (author) / Alag, G. (author) / Berry, P. (author) / Kotob, S. (author)

    Publication date :

    1974-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Digital adaptive flight controller development

    Kaufman, H. / Berry, P. | NTRS | 1973


    Digital adaptive flight controller development

    Kaufman, Howard | TIBKAT | 1974


    Digital Adaptive Flight Controller Development

    H. Kaufman / G. Alag / P. Berry et al. | NTIS | 1974