Passivity-Based Adaptive Internal Model Attitude Tracking Control of Uncertain Rigid Spacecraft

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

Abstract

The problems of a spacecraft attitude tracking and disturbance rejection are considered. Attitude tracking dynamics are formulated with typical Euler-Lagrange form, and a nonlinear controller is designed by combining a passivity-based adaptive method with an internal model. The unknown constant disturbance and inertia uncertainties are estimated online by element-wise adaptive update laws, while the unknown periodic disturbance is compensated by the internal model. Asymptotic stability of the closed-loop system is proved in the Lyapunov framework. A numerical example is also given to validate the theoretical results of this work.

Original languageEnglish
Title of host publicationProceedings of the 37th Chinese Control Conference, CCC 2018
EditorsXin Chen, Qianchuan Zhao
PublisherIEEE Computer Society
Pages9742-9747
Number of pages6
ISBN (Electronic)9789881563941
DOIs
StatePublished - 5 Oct 2018
Event37th Chinese Control Conference, CCC 2018 - Wuhan, China
Duration: 25 Jul 201827 Jul 2018

Publication series

NameChinese Control Conference, CCC
Volume2018-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference37th Chinese Control Conference, CCC 2018
Country/TerritoryChina
CityWuhan
Period25/07/1827/07/18

Keywords

  • Attitude tracking
  • Disturbance rejection
  • Internal model control
  • Passivity-based adaptive control
  • Spacecraft control

Fingerprint

Dive into the research topics of 'Passivity-Based Adaptive Internal Model Attitude Tracking Control of Uncertain Rigid Spacecraft'. Together they form a unique fingerprint.

Cite this