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Characteristic Model Based Robust HControl for Spacecraft Rendezvous and Proximity Operations

  • Beihang University

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

Abstract

An integrated motion control strategy for spacecraft rendezvous and proximity operations with parametric uncertainties, disturbances and couplings is presented in this paper. Firstly, the characteristic model of relative motion is established. By virtue of the obtained characteristic model, a robust H∞ relative translational and rotational controller is derived. Correspondingly, the controller design for spacecraft relative motion is formulated as a linear matrix inequality condition. Compared with previous integrated translational and rotational control schemes of spacecraft, the control strategy in this paper is easier to obtain without relying on precise mathematical model of the plant, and can guarantee the system performance subject to disturbances and parametric uncertainties. Numerical simulation verification indicates the effectiveness of the developed controller.

Original languageEnglish
Title of host publicationProceedings of the 40th Chinese Control Conference, CCC 2021
EditorsChen Peng, Jian Sun
PublisherIEEE Computer Society
Pages7683-7688
Number of pages6
ISBN (Electronic)9789881563804
DOIs
StatePublished - 26 Jul 2021
Event40th Chinese Control Conference, CCC 2021 - Shanghai, China
Duration: 26 Jul 202128 Jul 2021

Publication series

NameChinese Control Conference, CCC
Volume2021-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference40th Chinese Control Conference, CCC 2021
Country/TerritoryChina
CityShanghai
Period26/07/2128/07/21

Keywords

  • Characteristic Model
  • Relative Motion
  • Rendezvous and Proximity Operations
  • Robust HControl

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