Elsevier

Automatica

Volume 32, Issue 5, May 1996, Pages 669-677
Automatica

Paper
Explicit feedbacks stabilizing the attitude of a rigid spacecraft with two control torques

https://doi.org/10.1016/0005-1098(95)00194-8Get rights and content

Abstract

We construct explicit time-varying feedbacks that locally asymptotically stabilize the attitude of a rigid spacecraft with two controls.

References (40)

  • L. Rosier

    Inverse of Lyapunov's second theorem for measurable functions

  • H.J. Sussmann et al.

    Controllability of nonlinear systems

    J. Diff. Eqns

    (1972)
  • B. Bonnard

    Contrôle de l'attitude d'un satellite rigide

    RAIRO. Autom./Syst. Anal. Control

    (1982)
  • R.W. Brockett

    Asymptotic stability and feedback stabilization

  • C.I. Byrnes et al.

    Heuristics for nonlinear control

  • J.-M. Coron

    On the stabilization in finite time of locally controllable systems by means of continuous time-varying feedback laws

    SIAM J. Control Optim.

    (1995)
  • J.-M. Coron et al.

    A relation between continuous time-varying and discontinuous feedback stabilization

    J. Math. Syst., Estim. Control

    (1994)
  • P.E. Crouch

    Spacecraft attitude control and stabilization: applications of geometric control theory to rigid body models

    IEEE Trans. Autom. Control

    (1984)
  • P.E. Crouch et al.

    On sufficient conditions for local asymptotic stability of nonlinear systems whose linearization is uncontrollable

  • A. Filippov
  • Cited by (0)

    This paper was not presented at any IFAC meeting. This paper was recommended for publication in revised form by Associate Editor H. Logemann under the direction of Editor Ruth F. Curtain.

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