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. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Digital Adaptive Flight Controller Development


    Beteiligte:
    H. Kaufman (Autor:in) / G. Alag (Autor:in) / P. Berry (Autor:in) / S. Kotob (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    123 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Digital adaptive flight controller development

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


    Digital adaptive flight controller development

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


    Digital adaptive flight controller development

    Kaufman, Howard | TIBKAT | 1974