Skip to main navigation Skip to search Skip to main content

Adaptive pose tracking control for on-orbit tumbling target spacecraft

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

Abstract

It is assumed in this paper that the service spacecraft perform autonomous rendezvous and proximity operation to a tumbling target in space. Under this background, this paper proposes a relative coupled position and attitude dynamics. Using a Lyapunov framework, an adaptive controller is designed with the mass property of the service spacecraft uncertain. Numerical simulation is finally provided to illustrate the performance of the proposed controller.

Original languageEnglish
Title of host publicationProceedings - 5th International Conference on Instrumentation and Measurement, Computer, Communication, and Control, IMCCC 2015
EditorsJun-Bao Li
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1972-1976
Number of pages5
ISBN (Electronic)9781467377232
DOIs
StatePublished - 11 Feb 2016
Externally publishedYes
Event5th International Conference on Instrumentation and Measurement, Computer, Communication, and Control, IMCCC 2015 - Qinhuangdao, China
Duration: 18 Sep 201520 Sep 2015

Publication series

NameProceedings - 5th International Conference on Instrumentation and Measurement, Computer, Communication, and Control, IMCCC 2015

Conference

Conference5th International Conference on Instrumentation and Measurement, Computer, Communication, and Control, IMCCC 2015
Country/TerritoryChina
CityQinhuangdao
Period18/09/1520/09/15

Keywords

  • Adptive control
  • Autonomous rendezvous
  • Dual quaternion
  • Mass property
  • Pose coupling

Fingerprint

Dive into the research topics of 'Adaptive pose tracking control for on-orbit tumbling target spacecraft'. Together they form a unique fingerprint.

Cite this