On-orbit identification of disturbance torques acting on satellite with rotating payloads

Maoliang Chen, Yingying Liu, Jing Lei, Jun Zhou

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

1 Scopus citations

Abstract

This paper presents an approach to improve the stability of three-axis stabilized satellite with rotating payloads from a disturbance identification perspective. Based on steady-state output-only and the system transfer function, the unknown external and internal disturbance torques are identified in a closed loop without persistent excitation. The modified eigensystem identification algorithm(ERA) and the least-squares(LSM) method are employed to obtain the complete models of the disturbance torques. Finally, a feedforward control algorithm is proposed to achieve on-line compensation for the identified disturbance torques. Simulation results show that the approach proposed in this paper can reject the unknown and unwanted disturbance torques effectively, and improve the control performance of satellite with rotating payloads.

Original languageEnglish
Title of host publication2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009
Pages1342-1346
Number of pages5
DOIs
StatePublished - 2009
Event2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009 - Changchun, China
Duration: 9 Aug 200912 Aug 2009

Publication series

Name2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009

Conference

Conference2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009
Country/TerritoryChina
CityChangchun
Period9/08/0912/08/09

Keywords

  • Disturbance torques identification
  • Feedforward control
  • Least-squares method(LSM)
  • Modified eigensystem realization algorithm(ERA)
  • Rotating payloads

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