Comments on the paper: Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control

著录项

• 来源
  《Aerospace science and technology》 |2011年第3期|p.193-195|共3页
• 作者

  Shihua Li; Zhao Wang; Shumin Fei;

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• 作者单位

  Key Laboratory of Measurement and Control of Complex Systems of Engineering, Ministry of Education, School of Automation, Southeast University, Nanjing 210096, PR China;

  College of Information and Control Engineering, China University of Petroleum, Dongying 257061, PR China;

  Key Laboratory of Measurement and Control of Complex Systems of Engineering, Ministry of Education, School of Automation, Southeast University, Nanjing 210096, PR China;

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• 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  attitude tracking; rigid spacecraft; terminal sliding mode control;

  机译：姿态跟踪;刚性航天器;终端滑模控制;