Internal disturbance accommodation filter of control moment gyros with adaptive observer

Masaki Takahashi, Seiichi Shimizu, Shigemune Taniwaki, Kazuo Yoshida, Yoshiaki Ohkami

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The objective of this study is to establish the high accurate pointing control method of the satellite with CMG while taking a photograph of the ground target. In the method, after the satellite starts to maneuver, the frequency of the CMG internal disturbance is estimated by the adaptive observer of Kreisselmeier. After the maneuver of satellite is finished, the active internal disturbance accommodation filter based on the internal model principle is performed and thereby the internal disturbance is eliminated by feedforward control. From the simulation results, it was confirmed the usefulness of the proposed method.

Original languageEnglish
Title of host publicationAstrodynamics 2007 - Advances in the Astronautical Sciences, Proceedings of the AAS/AIAA Astrodynamics Specialist Conference
Pages1397-1411
Number of pages15
Publication statusPublished - 2008 Dec 1

Publication series

NameAdvances in the Astronautical Sciences
Volume129 PART 2
ISSN (Print)0065-3438

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

Fingerprint Dive into the research topics of 'Internal disturbance accommodation filter of control moment gyros with adaptive observer'. Together they form a unique fingerprint.

  • Cite this

    Takahashi, M., Shimizu, S., Taniwaki, S., Yoshida, K., & Ohkami, Y. (2008). Internal disturbance accommodation filter of control moment gyros with adaptive observer. In Astrodynamics 2007 - Advances in the Astronautical Sciences, Proceedings of the AAS/AIAA Astrodynamics Specialist Conference (pp. 1397-1411). (Advances in the Astronautical Sciences; Vol. 129 PART 2).