A Second-Order Sliding Mode Controller Design for Spacecraft Tracking Control
2013 ◽
Vol 2013
◽
pp. 1-9
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Keyword(s):
For spacecraft attitude tracking system, there exists the chattering phenomenon. In this paper, the spacecraft motion is decomposed into three-channel subsystems, and a second-order sliding mode control is proposed. This method has been proved to have good convergence and robustness. Combined with the proposed sliding surface, the three-channel controllers are designed. The control performance is confirmed by the simulation results, the approaching process is improved effectively, and a smooth transition is achieved without overshoot and buffeting.
Keyword(s):
2019 ◽
Vol 33
(1)
◽
pp. 61-73
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2013 ◽
Vol 27
(1)
◽
pp. 199-205
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Keyword(s):
2020 ◽
Vol 63
(3)
◽
pp. 213