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Adaptive integral-type sliding mode control for spacecraft attitude maneuvering under actuator stuck
  • 期刊名称：Chinese Journal of Aeronautics
  • 时间：2011.1.1
  • 页码：32-45
  • 相关项目：航天器执行器故障的输出反馈容错控制研究
作者： Qinglei Hu|Zhang Youmin|Xing Huo|
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航天器执行器故障的输出反馈容错控制研究
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