Journal
OPTIMIZATION AND ENGINEERING
Volume 4, Issue 3, Pages 215-230Publisher
SPRINGER
DOI: 10.1023/A:1023941231062
Keywords
path generation; under-actuated satellite; nonlinear discrete-time control; nonlinear predictive control
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An algorithm is proposed that performs a fast generation of trajectories that steer the state of an under-actuated satellite from a given initial value to the neighborhood of a final desired one. The proposed algorithm is then used to design a sampled-data state feedback control. Finally, simulations are proposed to test the robustness of the closed-loop behaviour under several classes of uncertainties and disturbances.
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