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Relative position and attitude coupled controller design for approaching and docking with a freely tumbling target

  • Bo Yan Jiang*
  • , Qing Lei Hu
  • , Zhong Shi
  • , Guang Fu Ma
  • *此作品的通讯作者
  • Harbin Institute of Technology
  • Civil Aviation University of China
  • Binzhou Polytechnic

科研成果: 期刊稿件文章同行评审

摘要

Relative position and attitude coupled control algorithm combined with sliding mode and adaptive control techniques is developed for an approaching and docking autonomously system, in which the unexpected disturbances and configuration uncertainties are considered explicitly. It is noted that the proposed controller can rigorously enforces actuator-magnitude saturation constraints and make the closed-loop system attenuate the disturbance with L2 gain. The associated stability proof is constructive and accomplished by the development of a novel Lyapunov function candidate. Numerical results show that this method achieves good tracking performance under the multi-constraints mentioned above.

源语言英语
页(从-至)54-60
页数7
期刊Yuhang Xuebao/Journal of Astronautics
35
1
DOI
出版状态已出版 - 1月 2014
已对外发布

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