Active formation along an eccentric orbit

Mai Bando, Akira Ichikawa

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

抄録

In this paper, a formation problem of a spacecraft with a leader in an elliptic orbit is considered, where the follower is required to track asymptotically a given periodic relative orbit. The linearized equations of relative motion along an eccentric orbit are known as Tschauner-Hempel equations. The Tschauner-Hempel equations are transformed into simpler ones by the change of variables. For the transformed system, the active formation problem is formulated, and feedback controllers are designed by the regulator equations associated with the Hill-Clohessy-Wiltshire equations. Feedback controllers are also designed using a DRE associated with the TH equations, and the Li-norms of designed controllers are compared.

本文言語英語
ホスト出版物のタイトル18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings
出版社IFAC Secretariat
ページ362-367
ページ数6
PART 1
ISBN(印刷版)9783902661968
DOI
出版ステータス出版済み - 2010
外部発表はい
イベント18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Nara, 日本
継続期間: 9 6 20109 10 2010

出版物シリーズ

名前IFAC Proceedings Volumes (IFAC-PapersOnline)
番号PART 1
18
ISSN(印刷版)1474-6670

その他

その他18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010
国/地域日本
CityNara
Period9/6/109/10/10

All Science Journal Classification (ASJC) codes

  • 制御およびシステム工学

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