Title :
Structurally stable attitude tracking for rigid spacecraft with parameter uncertainties
Author :
Toledo, B. Castillo ; Gennaro, S. Di
Author_Institution :
Centro de Investigacion y de Estudios Avanzados, IPN, Jalisco, Mexico
Abstract :
The paper deals with trajectory tracking for a rigid spacecraft under parameter uncertainties. This problem can be formulated as a structurally stable regulation problem. The reference inputs are generated by an autonomous system, the so-called exosystem. The solution of this problem entails the solution of the regulation equations, while the fulfillment of the robust requirement implies the immersion of the exosystem into observable system. Such an immersion allows all the possible steady-state inputs to be generated for the admissible values of the system parameters.
Keywords :
attitude control; matrix algebra; nonlinear control systems; robust control; space vehicles; tracking; uncertain systems; attitude tracking; autonomous system; exosystem; inertia matrix; nonlinear control; observable system; parameter uncertainties; rigid spacecraft; robust control; steady state inputs; structurally stable regulation problem; trajectory tracking; Adaptive control; Control systems; Output feedback; Robust control; Robustness; Space vehicles; Steady-state; Trajectory; Uncertain systems; Uncertainty;
Conference_Titel :
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
Print_ISBN :
0-7803-7516-5
DOI :
10.1109/CDC.2002.1185006
