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Finite-time control for nonlinear spacecraft attitude based on terminal sliding mode technique

Zhankui Song1, Hongxing Li1, Kaibiao Sun1

  • 1Faculty of Electroric Information and Electrical Engineering, Dalian University of Technology, Dalian 116024, PR China.

ISA Transactions
|September 24, 2013
PubMed

Keywords:
Double closed loopsFast terminal sliding mode controlFinite timeSpacecraft attitude control

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