Skip to main navigation Skip to search Skip to main content

Observer-based impulsive stabilization for spacecraft rendezvous

  • Harbin Institute of Technology

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

Abstract

This paper addresses the problem of observer-based impulsive stabilization for spacecraft rendezvous. An observer-based control strategy is developed to solve the stabilization problem in the presences of parameter uncertainty and variance constraint. Sufficient condition for the existence of the proposed controller is provided, and the controller synthesis problems are solved via linear matrix inequalities approach. Finally, a numerical example is established to demonstrate the effectiveness of the proposed control approach.

Original languageEnglish
Title of host publicationProceedings of the 28th Chinese Control and Decision Conference, CCDC 2016
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages3732-3736
Number of pages5
ISBN (Electronic)9781467397148
DOIs
StatePublished - 3 Aug 2016
Event28th Chinese Control and Decision Conference, CCDC 2016 - Yinchuan, China
Duration: 28 May 201630 May 2016

Publication series

NameProceedings of the 28th Chinese Control and Decision Conference, CCDC 2016

Conference

Conference28th Chinese Control and Decision Conference, CCDC 2016
Country/TerritoryChina
CityYinchuan
Period28/05/1630/05/16

Keywords

  • Impulse control and Observer-based control
  • Rendezvous
  • Spacecraft

Fingerprint

Dive into the research topics of 'Observer-based impulsive stabilization for spacecraft rendezvous'. Together they form a unique fingerprint.

Cite this