Vector field path following for a stratospheric satellite

Tian Chen; Zewei Zheng; Ming Zhu; Zhe Wu

doi:10.1109/CCDC.2015.7162881

Vector field path following for a stratospheric satellite

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

Abstract

This paper addresses the path following of a stratospheric satellite with propulsion systems, which is effective to realize orbit keeping and transfer. An algorithm for accurate path following of stratospheric satellites is proposed based on the theories of vector field and sliding mode control. Firstly, the dynamic model of the satellite propulsion system is presented, in which a 6 degree-of-freedom (6-DOF) stratospheric satellite model is introduced. Secondly, the control algorithm is proposed, which includes vector-field-based guidance laws to guide the satellite towards the desired path, sliding mode controllers to reduce path-following errors into an acceptable range and a forward velocity controller to maintain a constant velocity. Finally, simulation results demonstrate the effectiveness of the proposed control algorithm.

Original language	English
Title of host publication	Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	5370-5377
Number of pages	8
ISBN (Electronic)	9781479970179
DOIs	https://doi.org/10.1109/CCDC.2015.7162881
State	Published - 17 Jul 2015
Event	27th Chinese Control and Decision Conference, CCDC 2015 - Qingdao, China Duration: 23 May 2015 → 25 May 2015

Publication series

Name	Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015

Conference

Conference	27th Chinese Control and Decision Conference, CCDC 2015
Country/Territory	China
City	Qingdao
Period	23/05/15 → 25/05/15

Keywords

Path Following
Sliding Mode Control
Stratospheric Satellite
Vector Field

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10.1109/CCDC.2015.7162881

Cite this

Chen, T., Zheng, Z., Zhu, M., & Wu, Z. (2015). Vector field path following for a stratospheric satellite. In Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015 (pp. 5370-5377). Article 7162881 (Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC.2015.7162881

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title = "Vector field path following for a stratospheric satellite",

abstract = "This paper addresses the path following of a stratospheric satellite with propulsion systems, which is effective to realize orbit keeping and transfer. An algorithm for accurate path following of stratospheric satellites is proposed based on the theories of vector field and sliding mode control. Firstly, the dynamic model of the satellite propulsion system is presented, in which a 6 degree-of-freedom (6-DOF) stratospheric satellite model is introduced. Secondly, the control algorithm is proposed, which includes vector-field-based guidance laws to guide the satellite towards the desired path, sliding mode controllers to reduce path-following errors into an acceptable range and a forward velocity controller to maintain a constant velocity. Finally, simulation results demonstrate the effectiveness of the proposed control algorithm.",

keywords = "Path Following, Sliding Mode Control, Stratospheric Satellite, Vector Field",

author = "Tian Chen and Zewei Zheng and Ming Zhu and Zhe Wu",

note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; 27th Chinese Control and Decision Conference, CCDC 2015 ; Conference date: 23-05-2015 Through 25-05-2015",

year = "2015",

month = jul,

day = "17",

doi = "10.1109/CCDC.2015.7162881",

language = "英语",

series = "Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015",

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

pages = "5370--5377",

booktitle = "Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015",

address = "美国",

}

Chen, T , Zheng, Z , Zhu, M & Wu, Z 2015, Vector field path following for a stratospheric satellite. in Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015., 7162881, Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015, Institute of Electrical and Electronics Engineers Inc., pp. 5370-5377, 27th Chinese Control and Decision Conference, CCDC 2015, Qingdao, China, 23/05/15. https://doi.org/10.1109/CCDC.2015.7162881

Vector field path following for a stratospheric satellite. / Chen, Tian ; Zheng, Zewei ; Zhu, Ming et al.
Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015. Institute of Electrical and Electronics Engineers Inc., 2015. p. 5370-5377 7162881 (Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015).

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

TY - GEN

T1 - Vector field path following for a stratospheric satellite

AU - Chen, Tian

AU - Zheng, Zewei

AU - Zhu, Ming

AU - Wu, Zhe

PY - 2015/7/17

Y1 - 2015/7/17

N2 - This paper addresses the path following of a stratospheric satellite with propulsion systems, which is effective to realize orbit keeping and transfer. An algorithm for accurate path following of stratospheric satellites is proposed based on the theories of vector field and sliding mode control. Firstly, the dynamic model of the satellite propulsion system is presented, in which a 6 degree-of-freedom (6-DOF) stratospheric satellite model is introduced. Secondly, the control algorithm is proposed, which includes vector-field-based guidance laws to guide the satellite towards the desired path, sliding mode controllers to reduce path-following errors into an acceptable range and a forward velocity controller to maintain a constant velocity. Finally, simulation results demonstrate the effectiveness of the proposed control algorithm.

AB - This paper addresses the path following of a stratospheric satellite with propulsion systems, which is effective to realize orbit keeping and transfer. An algorithm for accurate path following of stratospheric satellites is proposed based on the theories of vector field and sliding mode control. Firstly, the dynamic model of the satellite propulsion system is presented, in which a 6 degree-of-freedom (6-DOF) stratospheric satellite model is introduced. Secondly, the control algorithm is proposed, which includes vector-field-based guidance laws to guide the satellite towards the desired path, sliding mode controllers to reduce path-following errors into an acceptable range and a forward velocity controller to maintain a constant velocity. Finally, simulation results demonstrate the effectiveness of the proposed control algorithm.

KW - Path Following

KW - Sliding Mode Control

KW - Stratospheric Satellite

KW - Vector Field

UR - https://www.scopus.com/pages/publications/84945544348

U2 - 10.1109/CCDC.2015.7162881

DO - 10.1109/CCDC.2015.7162881

M3 - 会议稿件

AN - SCOPUS:84945544348

T3 - Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015

SP - 5370

EP - 5377

BT - Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 27th Chinese Control and Decision Conference, CCDC 2015

Y2 - 23 May 2015 through 25 May 2015

ER -

Chen T , Zheng Z , Zhu M , Wu Z. Vector field path following for a stratospheric satellite. In Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015. Institute of Electrical and Electronics Engineers Inc. 2015. p. 5370-5377. 7162881. (Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015). doi: 10.1109/CCDC.2015.7162881

Vector field path following for a stratospheric satellite

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