Attitude synchronization of a spacecraft formation without velocity measurement

A. Abdessameud; A. Tayebi

doi:10.1109/CDC.2008.4738745

Attitude synchronization of a spacecraft formation without velocity measurement

A. Abdessameud, A. Tayebi

School of Science, Engineering & Technology (Harrisburg)

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

26 Scopus citations

Abstract

We consider the quaternion-based attitude synchronization problem of multiple spacecraft without velocity measurements. First, we propose a leader-follower-type control scheme for the attitude synchronization of a spacecraft formation to a desired constant attitude (available only to a single spacecraft called the leader), while maintaining the same attitude during formation maneuvers. Second, we consider the consensus seeking problem, where, no reference attitude is specified, and all spacecraft are required to align their attitudes with the same (possibly time varying) final angular velocity. The communication flow between spacecraft is assumed to be bidirectional. Simulation results of a scenario of four spacecraft are provided to show the effectiveness of the proposed control scheme.

Original language	English (US)
Title of host publication	Proceedings of the 47th IEEE Conference on Decision and Control, CDC 2008
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	3719-3724
Number of pages	6
ISBN (Print)	9781424431243
DOIs	https://doi.org/10.1109/CDC.2008.4738745
State	Published - 2008
Event	47th IEEE Conference on Decision and Control, CDC 2008 - Cancun, Mexico Duration: Dec 9 2008 → Dec 11 2008

Publication series

Name	Proceedings of the IEEE Conference on Decision and Control
ISSN (Print)	0743-1546
ISSN (Electronic)	2576-2370

Other

Other	47th IEEE Conference on Decision and Control, CDC 2008
Country/Territory	Mexico
City	Cancun
Period	12/9/08 → 12/11/08

All Science Journal Classification (ASJC) codes

Control and Systems Engineering
Modeling and Simulation
Control and Optimization

Access to Document

10.1109/CDC.2008.4738745

Cite this

Abdessameud, A., & Tayebi, A. (2008). Attitude synchronization of a spacecraft formation without velocity measurement. In Proceedings of the 47th IEEE Conference on Decision and Control, CDC 2008 (pp. 3719-3724). Article 4738745 (Proceedings of the IEEE Conference on Decision and Control). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CDC.2008.4738745

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title = "Attitude synchronization of a spacecraft formation without velocity measurement",

abstract = "We consider the quaternion-based attitude synchronization problem of multiple spacecraft without velocity measurements. First, we propose a leader-follower-type control scheme for the attitude synchronization of a spacecraft formation to a desired constant attitude (available only to a single spacecraft called the leader), while maintaining the same attitude during formation maneuvers. Second, we consider the consensus seeking problem, where, no reference attitude is specified, and all spacecraft are required to align their attitudes with the same (possibly time varying) final angular velocity. The communication flow between spacecraft is assumed to be bidirectional. Simulation results of a scenario of four spacecraft are provided to show the effectiveness of the proposed control scheme.",

author = "A. Abdessameud and A. Tayebi",

year = "2008",

doi = "10.1109/CDC.2008.4738745",

language = "English (US)",

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series = "Proceedings of the IEEE Conference on Decision and Control",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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note = "47th IEEE Conference on Decision and Control, CDC 2008 ; Conference date: 09-12-2008 Through 11-12-2008",

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Abdessameud, A & Tayebi, A 2008, Attitude synchronization of a spacecraft formation without velocity measurement. in Proceedings of the 47th IEEE Conference on Decision and Control, CDC 2008., 4738745, Proceedings of the IEEE Conference on Decision and Control, Institute of Electrical and Electronics Engineers Inc., pp. 3719-3724, 47th IEEE Conference on Decision and Control, CDC 2008, Cancun, Mexico, 12/9/08. https://doi.org/10.1109/CDC.2008.4738745

Attitude synchronization of a spacecraft formation without velocity measurement. / Abdessameud, A.; Tayebi, A.
Proceedings of the 47th IEEE Conference on Decision and Control, CDC 2008. Institute of Electrical and Electronics Engineers Inc., 2008. p. 3719-3724 4738745 (Proceedings of the IEEE Conference on Decision and Control).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

TY - GEN

T1 - Attitude synchronization of a spacecraft formation without velocity measurement

AU - Abdessameud, A.

AU - Tayebi, A.

PY - 2008

Y1 - 2008

N2 - We consider the quaternion-based attitude synchronization problem of multiple spacecraft without velocity measurements. First, we propose a leader-follower-type control scheme for the attitude synchronization of a spacecraft formation to a desired constant attitude (available only to a single spacecraft called the leader), while maintaining the same attitude during formation maneuvers. Second, we consider the consensus seeking problem, where, no reference attitude is specified, and all spacecraft are required to align their attitudes with the same (possibly time varying) final angular velocity. The communication flow between spacecraft is assumed to be bidirectional. Simulation results of a scenario of four spacecraft are provided to show the effectiveness of the proposed control scheme.

AB - We consider the quaternion-based attitude synchronization problem of multiple spacecraft without velocity measurements. First, we propose a leader-follower-type control scheme for the attitude synchronization of a spacecraft formation to a desired constant attitude (available only to a single spacecraft called the leader), while maintaining the same attitude during formation maneuvers. Second, we consider the consensus seeking problem, where, no reference attitude is specified, and all spacecraft are required to align their attitudes with the same (possibly time varying) final angular velocity. The communication flow between spacecraft is assumed to be bidirectional. Simulation results of a scenario of four spacecraft are provided to show the effectiveness of the proposed control scheme.

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SN - 9781424431243

T3 - Proceedings of the IEEE Conference on Decision and Control

SP - 3719

EP - 3724

BT - Proceedings of the 47th IEEE Conference on Decision and Control, CDC 2008

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 47th IEEE Conference on Decision and Control, CDC 2008

Y2 - 9 December 2008 through 11 December 2008

ER -

Attitude synchronization of a spacecraft formation without velocity measurement

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All Science Journal Classification (ASJC) codes

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