Honeywell has designed a digital self-adaptive flight control system for flight test in the VALT Research Aircraft (a modified CH-47). The final design resulted from a comparison of two different adaptive concepts: one based on explicit parameter estimates from a real-time maximum likelihood estimation algorithm and the other based on an implicit model reference adaptive system. The two designs are compared on the basis of performance and complexity.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Digital adaptive control laws for VTOL aircraft


    Beteiligte:
    Hartmann, G. L. (Autor:in) / Stein, G. (Autor:in)

    Kongress:

    1978 Conference on Decision and Control ; 1979 ; San Diego, CA


    Erscheinungsdatum :

    01.01.1979


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    AUTOLAND SYSTEM FOR VTOL AIRCRAFT, VTOL AIRCRAFT, AND LANDING CONTROL METHOD FOR VTOL AIRCRAFT

    KOJIMA TORU / MORI SATOSHI | Europäisches Patentamt | 2024

    Freier Zugriff

    Digital controllers for VTOL aircraft

    Stengel, R.F. / Broussard, J.R. / Berry, P.W. | Tema Archiv | 1978


    Digital controllers for VTOL aircraft

    Stengel, R. F. / Broussard, J. R. / Berry, P. W. | NTRS | 1976


    Digital Controllers for VTOL Aircraft

    Stengel, Robert F. / Broussard, John R. / Berry, Paul W. | IEEE | 1978


    The design of digital-adaptive controllers for VTOL aircraft

    Stengel, R. F. / Broussard, J. R. / Berry, P. W. | NTRS | 1976