An examination of two aircraft controller structures applicable to on-line implementation was conducted. The two controllers, a linear regulator model follower and an inner-product model follower, were applied to the lateral dynamics of the F8-C aircraft. For the purposes of this research effort, the lateral dynamics of the F8-C aircraft were considered. The controller designs were evaluated for four flight conditions. Additionally, effects of pilot input, rapid variation of flight condition and control surface rate and magnitude deflection limits were considered.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Optimal controller design for high performance aircraft undergoing large disturbance angles


    Beteiligte:
    Rhoten, R. P. (Autor:in)

    Erscheinungsdatum :

    1974-02-28


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Disturbance Observer Based Sliding Mode Controller Design for Large Civil Aircraft

    Zeng, Chao / Tsourdos, Antonios / Lone, Mohammad M. | AIAA | 2013


    Disturbance Observer Based Sliding Mode Controller Design for Large Civil Aircraft (AIAA 2013-4694)

    Chao, Z. / Tsourdos, A. / Lone, M.M. et al. | British Library Conference Proceedings | 2013


    LQR Aircraft pitch controller design for handling disturbance using differential evolution

    Kanokmedhakul, Y. / Pholdee, N. / Bureerat, S. et al. | BASE | 2019

    Freier Zugriff

    Optimal design of the aircraft ABS controller

    Ko, H.Y. / Ha, D.J. / Choi, N.Y. | Tema Archiv | 2003