This paper will describe the results of an ongoing investigation into controller design for the rejection of atmospheric turbulence. The gust disturbance is considered as an extra input to the well-known H∞ mixed sensitivity design formulation. Results from the nonlinear simulations are presented, and these show significant improvement in the helicopters performance.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Rotorcraft control law design for rejection of atmospheric turbulence


    Beteiligte:
    Postlethwaite, I. (Autor:in) / Foster, N.P. (Autor:in) / Walker, D.J. (Autor:in)

    Erscheinungsdatum :

    01.01.1994


    Format / Umfang :

    6 pages



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Rotorcraft control system design for rejection of atmospheric turbulence

    Foster, N. P. / Postlethwaite, I. / Walker, D. J. et al. | British Library Conference Proceedings | 1994


    Rotorcraft responses to atmospheric turbulence

    Gool, Paul Cornelius Antonius | TIBKAT | 1997


    Atmospheric turbulence simulation for rotorcraft applications

    Riaz, J. / Prasad, J. V. R. / Schrage, D. P. et al. | NTRS | 1993


    Atmospheric turbulence simulation for rotorcraft applications

    Riaz, J. / Prasad, J.V.R. / Schrage, D.P. et al. | Tema Archiv | 1993


    A new method for simulating atmospheric turbulence for rotorcraft applications

    Prasad, J. V. R. / Schrage, D. P. / Gaonkar, G. H. et al. | NTRS | 1991