Backstepping sliding mode control for combined spacecraft with nonlinear disturbance observer

Han Gao, Yueyong Lv, Guangfu Ma, Chuanjiang Li

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

10 Citations (Scopus)

Abstract

To attenuate the effects of inertia uncertainty and external disturbance of combined spacecraft on attitude control accuracy and stability, a composite control law by combining nonlinear disturbance observer (NDO) and backstepping sliding mode control is proposed. In this paper, the nonlinear disturbance observer (NDO) is added to observe the unknown inertia and external disturbance, and asymptotic stability of the backstepping sliding mode control with NDO is demonstrated. The performance of the proposed attitude control for combined spacecraft is discussed, and the simulation results demonstrate the effectiveness and feasibility of the proposed controller.

Original languageEnglish
Title of host publication2016 UKACC International Conference on Control, UKACC Control 2016
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781467398916
DOIs
Publication statusPublished - 7 Nov 2016
Externally publishedYes
Event11th UKACC United Kingdom Automatic Control Council International Conference on Control, UKACC Control 2016 - Belfast, United Kingdom
Duration: 31 Aug 20162 Sept 2016

Publication series

Name2016 UKACC International Conference on Control, UKACC Control 2016

Conference

Conference11th UKACC United Kingdom Automatic Control Council International Conference on Control, UKACC Control 2016
Country/TerritoryUnited Kingdom
CityBelfast
Period31/08/162/09/16

Keywords

  • backstepping
  • combined spacecraft
  • nonlinear disturbance observer
  • sliding mode

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