Robust nonlinear control for spacecraft rendezvous and docking with disturbance observer

Kewei Xia, Wei Huo*

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

3 Citations (Scopus)

Abstract

This paper presents a robust nonlinear control strategy for a cooperative spacecraft rendezvous and docking maneuver with coupled attitude and position dynamics. The nonlinear and coupled models of relative attitude and relative position motions are expressed in the pursuer body-fixed frame, respectively. Both parametric uncertainties and disturbances are estimated together by a second-order nonlinear disturbance observer. A robust control strategy based on feedback linearization is developed. It is proved that the states of the closed loop systems are uniformly ultimately bounded in presence of parametric uncertainties and disturbances by using Lyapunov theory. Theoretical conclusions are demonstrated by numerical simulations.

Original languageEnglish
Title of host publicationProceedings of the 35th Chinese Control Conference, CCC 2016
EditorsJie Chen, Qianchuan Zhao, Jie Chen
PublisherIEEE Computer Society
Pages398-403
Number of pages6
ISBN (Electronic)9789881563910
DOIs
Publication statusPublished - 26 Aug 2016
Externally publishedYes
Event35th Chinese Control Conference, CCC 2016 - Chengdu, China
Duration: 27 Jul 201629 Jul 2016

Publication series

NameChinese Control Conference, CCC
Volume2016-August
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference35th Chinese Control Conference, CCC 2016
Country/TerritoryChina
CityChengdu
Period27/07/1629/07/16

Keywords

  • Disturbance observer
  • Nonlinear control
  • Rendezvous and docking
  • Spacecraft control

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