Physical simulation experiment for flexible satellite control with accelerometer

Ying Ying Liu, Jun Zhou, Jian Zhao Din

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

1 Scopus citations

Abstract

The dynamic model of a physical simulation experiment system for flexible satellites is given. The measurement model of the accelerometer placed at the end of the flexible panel is established and an adaptive filter is used for its data procession. Feedback control using vibration information got from the accelerometer signal is designed, and physical simulation experiment results show that the control scheme is effective in vibration suppression.

Original languageEnglish
Title of host publication2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
Pages1020-1024
Number of pages5
DOIs
StatePublished - 2006
Event2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006 - Luoyang, China
Duration: 25 Jun 200628 Jun 2006

Publication series

Name2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
Volume2006

Conference

Conference2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006
Country/TerritoryChina
CityLuoyang
Period25/06/0628/06/06

Keywords

  • Accelerometer signal
  • Flexible satellite
  • Physical simulation experiment
  • Vibration suppression

Fingerprint

Dive into the research topics of 'Physical simulation experiment for flexible satellite control with accelerometer'. Together they form a unique fingerprint.

Cite this