PaperExplicit feedbacks stabilizing the attitude of a rigid spacecraft with two control torques☆
References (40)
Stabilization by smooth feedback of the angular velocity of a rigid body
Syst. Control Lett.
(1985)- et al.
Comments on the stabilizability of the angular velocity of a rigid body
Syst. Control Lett.
(1988) Stabilization with relaxed controls
Nonlinear Anal., Theory, Meth., Applic.
(1983)- et al.
New results and examples in nonlinear feedback stabilization
Syst. Control Lett.
(1989) - et al.
On the attitude stability of rigid spacecraft
Automatica
(1991) Links between local controllability and local continuous stabilization
- et al.
Adding an integrator for the stabilization problem
Syst. Control Lett.
(1991) - et al.
Stabilizability of the angular velocity of a rigid body
Syst. Control Lett.
(1992) - et al.
Time-varying feedback stabilization of the attitude of a rigid spacecraft with two controls
Syst. Control Lett.
(1995) Homogeneous Lyapunov function for continuous vector field
Syst. Control Lett.
(1992)
Inverse of Lyapunov's second theorem for measurable functions
Controllability of nonlinear systems
J. Diff. Eqns
(1972)
Contrôle de l'attitude d'un satellite rigide
RAIRO. Autom./Syst. Anal. Control
(1982)
Asymptotic stability and feedback stabilization
Heuristics for nonlinear control
On the stabilization in finite time of locally controllable systems by means of continuous time-varying feedback laws
SIAM J. Control Optim.
(1995)
A relation between continuous time-varying and discontinuous feedback stabilization
J. Math. Syst., Estim. Control
(1994)
Spacecraft attitude control and stabilization: applications of geometric control theory to rigid body models
IEEE Trans. Autom. Control
(1984)
On sufficient conditions for local asymptotic stability of nonlinear systems whose linearization is uncontrollable
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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.
Copyright © 1996 Published by Elsevier Ltd.