The nonlinear set of equations which represent helicopter motion is linearized about a prescribed nominal state. Once the linearized system is obtained it is validated by comparing the output of the nonlinear system to that of its linearized counterpart. Having obtained a linear model, linear system theory may then be applied in order to investigate the stability and control characteristics of the aircraft.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Helicopter motion: equation linearization


    Weitere Titelangaben:

    Hubschrauber-Bewegung: Gleichungslinearisierung


    Beteiligte:
    Fermelia, A. (Autor:in) / Gyorog, D.A. (Autor:in) / Flanigan, V.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976


    Format / Umfang :

    16 Seiten, 5 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Helicopter Motion: Equation Linearization

    Fermelia, A. / Gyorog, D. A. / Flanigan, V. J. | IEEE | 1976


    Helicopter control design using feedback linearization techniques

    Liceaga-Castro, E. / Bradley, R. / Castro-Linares, R. | Tema Archiv | 1989


    Helicopter Robust Nonlinear Controller Synthesis Using Approximate Linearization

    Leitner, J. / Prasad, J. V. R. / American Helicopter Society | British Library Conference Proceedings | 1993


    Adaptive feedback linearization flight control for a helicopter UAV

    Bijnens, Bert / Chu, Q.P. / Voorsluijs, Gerwin et al. | AIAA | 2005


    Yaw Control of an Unmanned Helicopter with Feedback Linearization

    Mohammadzahei, Morteza / Ziaiefar, Hamidreza / Ghodsi, Mojtaba et al. | IEEE | 2019