It is shown that, by incorporating fast on-line recursive identifiers to provide updated step-response matrices for inclusion in digital PID control laws, highly effective adaptive digital set-point tracking controllers can be readily designed for multivariable plants. The effectiveness of such an adaptive controller is illustrated by the design of an adaptive direct digital flight-mode control system for the F-16 aircraft.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Design of adaptive direct digital flight-mode control systems incorporating recursive step-response matrix identifiers for high-performance aircraft


    Additional title:

    Entwurf von adpativen, digitalen Flugregelsystemen unter Einbeziehung von rekursiven Identifikatoren fuer Hochleistungsflugzeuge


    Contributors:
    Porter, B. (author) / Manganas, A. (author)


    Publication date :

    1986


    Size :

    6 Seiten, 12 Bilder, 6 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English