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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
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Civil Aviation University of China
  • Binzhou Polytechnic

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Original languageEnglish
Pages (from-to)54-60
Number of pages7
JournalYuhang Xuebao/Journal of Astronautics
Volume35
Issue number1
DOIs
StatePublished - Jan 2014
Externally publishedYes

Keywords

  • Control saturation
  • Coupled control
  • L disturbance attenuation
  • Rendezvous and docking

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