Safe approaching to non-cooperative spacecraft using potential function guidance based fuzzy logic system

Dawei Zhang; Shenmin Song; Run Pei; Baoqun Zhang

doi:10.1109/WCICA.2010.5553862

Safe approaching to non-cooperative spacecraft using potential function guidance based fuzzy logic system

Dawei Zhang^*
, Shenmin Song
, Run Pei
, Baoqun Zhang

^*Corresponding author for this work

School of Astronautics, Harbin Institute of Technology

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

7 Scopus citations

Abstract

A guidance control method is proposed for the mission of autonomous rendezvous and docking with non-cooperative target spacecraft. Firstly, the relative motion equations of state are described in a line of sight coordinate frame. Then artificial potential function guidance is used for chaser to approach non-cooperative target. Moreover, this guidance method is based on fuzzy logic system which satisfies safe approaching constraints in final approaching corridor scenario between the two spacecrafts. Stability of the proposed method is analyzed by using Lyapunov theory. Results obtained from numerical simulation studies demonstrate the validity of the method formulated in this paper.

Original language	English
Title of host publication	2010 8th World Congress on Intelligent Control and Automation, WCICA 2010
Pages	3526-3531
Number of pages	6
DOIs	https://doi.org/10.1109/WCICA.2010.5553862
State	Published - 2010
Externally published	Yes
Event	2010 8th World Congress on Intelligent Control and Automation, WCICA 2010 - Jinan, China Duration: 7 Jul 2010 → 9 Jul 2010

Publication series

Name	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

Conference

Conference	2010 8th World Congress on Intelligent Control and Automation, WCICA 2010
Country/Territory	China
City	Jinan
Period	7/07/10 → 9/07/10

Keywords

Artificial potential function guidance
Autonomous rendezvous and docking
Fuzzy logic system
Non-cooperative target
Safe approaching constraints

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10.1109/WCICA.2010.5553862

Cite this

Zhang, D., Song, S., Pei, R., & Zhang, B. (2010). Safe approaching to non-cooperative spacecraft using potential function guidance based fuzzy logic system. In 2010 8th World Congress on Intelligent Control and Automation, WCICA 2010 (pp. 3526-3531). Article 5553862 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA)). https://doi.org/10.1109/WCICA.2010.5553862

@inproceedings{3a037b82d0c34562bdf9626b85b99cc5,

title = "Safe approaching to non-cooperative spacecraft using potential function guidance based fuzzy logic system",

abstract = "A guidance control method is proposed for the mission of autonomous rendezvous and docking with non-cooperative target spacecraft. Firstly, the relative motion equations of state are described in a line of sight coordinate frame. Then artificial potential function guidance is used for chaser to approach non-cooperative target. Moreover, this guidance method is based on fuzzy logic system which satisfies safe approaching constraints in final approaching corridor scenario between the two spacecrafts. Stability of the proposed method is analyzed by using Lyapunov theory. Results obtained from numerical simulation studies demonstrate the validity of the method formulated in this paper.",

keywords = "Artificial potential function guidance, Autonomous rendezvous and docking, Fuzzy logic system, Non-cooperative target, Safe approaching constraints",

author = "Dawei Zhang and Shenmin Song and Run Pei and Baoqun Zhang",

year = "2010",

doi = "10.1109/WCICA.2010.5553862",

language = "英语",

isbn = "9781424467129",

series = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",

pages = "3526--3531",

booktitle = "2010 8th World Congress on Intelligent Control and Automation, WCICA 2010",

note = "2010 8th World Congress on Intelligent Control and Automation, WCICA 2010 ; Conference date: 07-07-2010 Through 09-07-2010",

}

Zhang, D, Song, S, Pei, R & Zhang, B 2010, Safe approaching to non-cooperative spacecraft using potential function guidance based fuzzy logic system. in 2010 8th World Congress on Intelligent Control and Automation, WCICA 2010., 5553862, Proceedings of the World Congress on Intelligent Control and Automation (WCICA), pp. 3526-3531, 2010 8th World Congress on Intelligent Control and Automation, WCICA 2010, Jinan, China, 7/07/10. https://doi.org/10.1109/WCICA.2010.5553862

Safe approaching to non-cooperative spacecraft using potential function guidance based fuzzy logic system. / Zhang, Dawei; Song, Shenmin; Pei, Run et al.
2010 8th World Congress on Intelligent Control and Automation, WCICA 2010. 2010. p. 3526-3531 5553862 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA)).

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

TY - GEN

T1 - Safe approaching to non-cooperative spacecraft using potential function guidance based fuzzy logic system

AU - Zhang, Dawei

AU - Song, Shenmin

AU - Pei, Run

AU - Zhang, Baoqun

PY - 2010

Y1 - 2010

N2 - A guidance control method is proposed for the mission of autonomous rendezvous and docking with non-cooperative target spacecraft. Firstly, the relative motion equations of state are described in a line of sight coordinate frame. Then artificial potential function guidance is used for chaser to approach non-cooperative target. Moreover, this guidance method is based on fuzzy logic system which satisfies safe approaching constraints in final approaching corridor scenario between the two spacecrafts. Stability of the proposed method is analyzed by using Lyapunov theory. Results obtained from numerical simulation studies demonstrate the validity of the method formulated in this paper.

AB - A guidance control method is proposed for the mission of autonomous rendezvous and docking with non-cooperative target spacecraft. Firstly, the relative motion equations of state are described in a line of sight coordinate frame. Then artificial potential function guidance is used for chaser to approach non-cooperative target. Moreover, this guidance method is based on fuzzy logic system which satisfies safe approaching constraints in final approaching corridor scenario between the two spacecrafts. Stability of the proposed method is analyzed by using Lyapunov theory. Results obtained from numerical simulation studies demonstrate the validity of the method formulated in this paper.

KW - Artificial potential function guidance

KW - Autonomous rendezvous and docking

KW - Fuzzy logic system

KW - Non-cooperative target

KW - Safe approaching constraints

UR - https://www.scopus.com/pages/publications/77958117016

U2 - 10.1109/WCICA.2010.5553862

DO - 10.1109/WCICA.2010.5553862

M3 - 会议稿件

AN - SCOPUS:77958117016

SN - 9781424467129

T3 - Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

SP - 3526

EP - 3531

BT - 2010 8th World Congress on Intelligent Control and Automation, WCICA 2010

T2 - 2010 8th World Congress on Intelligent Control and Automation, WCICA 2010

Y2 - 7 July 2010 through 9 July 2010

ER -

Safe approaching to non-cooperative spacecraft using potential function guidance based fuzzy logic system

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Keywords

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