Limited-thrust relative position holding for adjacent spacecraft with thruster nonlinearity

Xuebo Yang; Wei Wang; Huijun Gao

doi:10.1109/CDC.2011.6160556

Limited-thrust relative position holding for adjacent spacecraft with thruster nonlinearity

Xuebo Yang^*
, Wei Wang
, Huijun Gao

^*Corresponding author for this work

School of Astronautics

Dalian University of Technology

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

Abstract

The problem of spacecraft relative position holding with limited thrust and thruster nonlinearity is investigated in this paper. The relative dynamic model with sampled-data measurement is established based on the Clohessy-Wiltshire (C-W) equations. Thruster nonlinearity and limited thrust constraint are taken into consideration. Then, the relative position holding problem is regarded as a sampled-data output tracking control problem. Based on Lyapunov stabilization theory, the sampled-data controller is designed by solving a convex optimization problem. Simulations show the effectiveness of the proposed method.

Original language	English
Title of host publication	2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	8304-8308
Number of pages	5
ISBN (Print)	9781612848006
DOIs	https://doi.org/10.1109/CDC.2011.6160556
State	Published - 2011
Event	2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011 - Orlando, FL, United States Duration: 12 Dec 2011 → 15 Dec 2011

Publication series

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

Conference

Conference	2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011
Country/Territory	United States
City	Orlando, FL
Period	12/12/11 → 15/12/11

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10.1109/CDC.2011.6160556

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Yang, X., Wang, W., & Gao, H. (2011). Limited-thrust relative position holding for adjacent spacecraft with thruster nonlinearity. In 2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011 (pp. 8304-8308). Article 6160556 (Proceedings of the IEEE Conference on Decision and Control). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CDC.2011.6160556

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title = "Limited-thrust relative position holding for adjacent spacecraft with thruster nonlinearity",

abstract = "The problem of spacecraft relative position holding with limited thrust and thruster nonlinearity is investigated in this paper. The relative dynamic model with sampled-data measurement is established based on the Clohessy-Wiltshire (C-W) equations. Thruster nonlinearity and limited thrust constraint are taken into consideration. Then, the relative position holding problem is regarded as a sampled-data output tracking control problem. Based on Lyapunov stabilization theory, the sampled-data controller is designed by solving a convex optimization problem. Simulations show the effectiveness of the proposed method.",

author = "Xuebo Yang and Wei Wang and Huijun Gao",

year = "2011",

doi = "10.1109/CDC.2011.6160556",

language = "英语",

isbn = "9781612848006",

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

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

pages = "8304--8308",

booktitle = "2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011",

address = "美国",

note = "2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011 ; Conference date: 12-12-2011 Through 15-12-2011",

}

Yang, X, Wang, W & Gao, H 2011, Limited-thrust relative position holding for adjacent spacecraft with thruster nonlinearity. in 2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011., 6160556, Proceedings of the IEEE Conference on Decision and Control, Institute of Electrical and Electronics Engineers Inc., pp. 8304-8308, 2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011, Orlando, FL, United States, 12/12/11. https://doi.org/10.1109/CDC.2011.6160556

Limited-thrust relative position holding for adjacent spacecraft with thruster nonlinearity. / Yang, Xuebo; Wang, Wei; Gao, Huijun.
2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011. Institute of Electrical and Electronics Engineers Inc., 2011. p. 8304-8308 6160556 (Proceedings of the IEEE Conference on Decision and Control).

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

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AU - Yang, Xuebo

AU - Wang, Wei

AU - Gao, Huijun

PY - 2011

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N2 - The problem of spacecraft relative position holding with limited thrust and thruster nonlinearity is investigated in this paper. The relative dynamic model with sampled-data measurement is established based on the Clohessy-Wiltshire (C-W) equations. Thruster nonlinearity and limited thrust constraint are taken into consideration. Then, the relative position holding problem is regarded as a sampled-data output tracking control problem. Based on Lyapunov stabilization theory, the sampled-data controller is designed by solving a convex optimization problem. Simulations show the effectiveness of the proposed method.

AB - The problem of spacecraft relative position holding with limited thrust and thruster nonlinearity is investigated in this paper. The relative dynamic model with sampled-data measurement is established based on the Clohessy-Wiltshire (C-W) equations. Thruster nonlinearity and limited thrust constraint are taken into consideration. Then, the relative position holding problem is regarded as a sampled-data output tracking control problem. Based on Lyapunov stabilization theory, the sampled-data controller is designed by solving a convex optimization problem. Simulations show the effectiveness of the proposed method.

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DO - 10.1109/CDC.2011.6160556

M3 - 会议稿件

AN - SCOPUS:84860668042

SN - 9781612848006

T3 - Proceedings of the IEEE Conference on Decision and Control

SP - 8304

EP - 8308

BT - 2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011

Y2 - 12 December 2011 through 15 December 2011

ER -

Yang X, Wang W, Gao H. Limited-thrust relative position holding for adjacent spacecraft with thruster nonlinearity. In 2011 50th IEEE Conference on Decision and Control and European Control Conference, CDC-ECC 2011. Institute of Electrical and Electronics Engineers Inc. 2011. p. 8304-8308. 6160556. (Proceedings of the IEEE Conference on Decision and Control). doi: 10.1109/CDC.2011.6160556

Limited-thrust relative position holding for adjacent spacecraft with thruster nonlinearity

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