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Finite-time fault tolerant control for spacecraft using sliding mode method.

Lijun ZhangYuanqing XiaGanghui ShenKunfeng Lu
Published in: IECON (2017)
Keyphrases
  • stability analysis
  • neural network
  • least squares
  • convergence rate
  • dynamic programming
  • support vector machine
  • dynamic environments
  • optimization algorithm