A nonlinear control law design based upon the backstepping approach is addressed for attitude maneuver control of spacecraft by momentum transfer (MT) in the presence of disturbance. For MT, a traditional method usually applies constant torque as an input, which tends to produce significant residual oscillation. Enhanced methods such as optimal control can somewhat reduce the residual oscillation, but may not be enough for minimum residual motion. Feedback linearization technique can drive the final nutation angle small enough, but it is rather sensitive to parameter uncertainty. The proposed method here takes advantage of nonlinear control approach with small steady-state nutation angle. Sensitivity about parameter uncertainties by feedback linearization can be reduced by the backstepping technique. Stability of the resulting control law is guaranteed by the Lyapunov stability theory. Boundedness of the control law is presented to validate practical merit of the proposed control law.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Momentum transfer-based attitude control of spacecraft with backstepping


    Beteiligte:
    Baohua Lian, (Autor:in) / Hyochoong Bang, (Autor:in)


    Erscheinungsdatum :

    01.04.2006


    Format / Umfang :

    840515 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Momentum transfer-based attitude control of spacecraft with backstepping

    Lian, Baohua / Bang, Hyochoong | Tema Archiv | 2006



    PID+ backstepping control of relative spacecraft attitude

    Krogstad, Thomas R. / Kristiansen, Raymond / Gravdahl, Jan Tommy et al. | Tema Archiv | 2009


    Spacecraft attitude slew maneuver control via backstepping method

    Minjie, Z. / Shijie, X. | British Library Online Contents | 2007