Active formation along an eccentric orbit

Mai Bando, Akira Ichikawa

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

Abstract

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.

Original languageEnglish
Title of host publication18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings
PublisherIFAC Secretariat
Pages362-367
Number of pages6
EditionPART 1
ISBN (Print)9783902661968
Publication statusPublished - Jan 1 2010
Event18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Nara, Japan
Duration: Sep 6 2010Sep 10 2010

Publication series

NameIFAC Proceedings Volumes (IFAC-PapersOnline)
NumberPART 1
Volume18
ISSN (Print)1474-6670

Other

Other18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010
CountryJapan
CityNara
Period9/6/109/10/10

Fingerprint

Orbits
Controllers
Feedback
Spacecraft

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering

Cite this

Bando, M., & Ichikawa, A. (2010). Active formation along an eccentric orbit. In 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings (PART 1 ed., pp. 362-367). (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 18, No. PART 1). IFAC Secretariat.

Active formation along an eccentric orbit. / Bando, Mai; Ichikawa, Akira.

18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings. PART 1. ed. IFAC Secretariat, 2010. p. 362-367 (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 18, No. PART 1).

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

Bando, M & Ichikawa, A 2010, Active formation along an eccentric orbit. in 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings. PART 1 edn, IFAC Proceedings Volumes (IFAC-PapersOnline), no. PART 1, vol. 18, IFAC Secretariat, pp. 362-367, 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010, Nara, Japan, 9/6/10.
Bando M, Ichikawa A. Active formation along an eccentric orbit. In 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings. PART 1 ed. IFAC Secretariat. 2010. p. 362-367. (IFAC Proceedings Volumes (IFAC-PapersOnline); PART 1).
Bando, Mai ; Ichikawa, Akira. / Active formation along an eccentric orbit. 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings. PART 1. ed. IFAC Secretariat, 2010. pp. 362-367 (IFAC Proceedings Volumes (IFAC-PapersOnline); PART 1).
@inproceedings{3a3f9492bbd345be8076097bd0ba1f25,
title = "Active formation along an eccentric orbit",
abstract = "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.",
author = "Mai Bando and Akira Ichikawa",
year = "2010",
month = "1",
day = "1",
language = "English",
isbn = "9783902661968",
series = "IFAC Proceedings Volumes (IFAC-PapersOnline)",
publisher = "IFAC Secretariat",
number = "PART 1",
pages = "362--367",
booktitle = "18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings",
address = "Austria",
edition = "PART 1",

}

TY - GEN

T1 - Active formation along an eccentric orbit

AU - Bando, Mai

AU - Ichikawa, Akira

PY - 2010/1/1

Y1 - 2010/1/1

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=84901606365&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84901606365&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84901606365

SN - 9783902661968

T3 - IFAC Proceedings Volumes (IFAC-PapersOnline)

SP - 362

EP - 367

BT - 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings

PB - IFAC Secretariat

ER -