Parameter identification of spacecraft rendezvous under non-cooperative case

Guangren Duan; Xiuwei Huang; Gang Xu

doi:10.1109/ChiCC.2016.7553691

Parameter identification of spacecraft rendezvous under non-cooperative case

Guangren Duan
, Xiuwei Huang
, Gang Xu

School of Astronautics

Harbin Institute of Technology

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

Abstract

In this paper, the problem about parameter identification of spacecraft rendezvous under non-cooperative case is investigated. A new kind of identification method about continuous linear system is proposed. Firstly, linear transform algorithm and generalized bilinear transform algorithm as new discretization algorithms of continuous system are stated. According to these two algorithms, the parameters of continuous and discrete system can be connected by analytical way rather than approximate method, besides, their relationship is reversible. Then, by employing the MIMO recursive extended least squares algorithm, the spacecraft rendezvous system is identified. The simulation results show that the statistic errors of parameter following by two algorithms both converge to zero with the increase of the iteration steps and the latter algorithm has smaller parameter error.

Original language	English
Title of host publication	Proceedings of the 35th Chinese Control Conference, CCC 2016
Editors	Jie Chen, Qianchuan Zhao, Jie Chen
Publisher	IEEE Computer Society
Pages	2176-2181
Number of pages	6
ISBN (Electronic)	9789881563910
DOIs	https://doi.org/10.1109/ChiCC.2016.7553691
State	Published - 26 Aug 2016
Event	35th Chinese Control Conference, CCC 2016 - Chengdu, China Duration: 27 Jul 2016 → 29 Jul 2016

Publication series

Name	Chinese Control Conference, CCC
Volume	2016-August
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	35th Chinese Control Conference, CCC 2016
Country/Territory	China
City	Chengdu
Period	27/07/16 → 29/07/16

Keywords

C-W equation
Discretization algorithm
Non-cooperation
Parameter identification

Access to Document

10.1109/ChiCC.2016.7553691

Cite this

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title = "Parameter identification of spacecraft rendezvous under non-cooperative case",

abstract = "In this paper, the problem about parameter identification of spacecraft rendezvous under non-cooperative case is investigated. A new kind of identification method about continuous linear system is proposed. Firstly, linear transform algorithm and generalized bilinear transform algorithm as new discretization algorithms of continuous system are stated. According to these two algorithms, the parameters of continuous and discrete system can be connected by analytical way rather than approximate method, besides, their relationship is reversible. Then, by employing the MIMO recursive extended least squares algorithm, the spacecraft rendezvous system is identified. The simulation results show that the statistic errors of parameter following by two algorithms both converge to zero with the increase of the iteration steps and the latter algorithm has smaller parameter error.",

keywords = "C-W equation, Discretization algorithm, Non-cooperation, Parameter identification",

author = "Guangren Duan and Xiuwei Huang and Gang Xu",

note = "Publisher Copyright: {\textcopyright} 2016 TCCT.; 35th Chinese Control Conference, CCC 2016 ; Conference date: 27-07-2016 Through 29-07-2016",

year = "2016",

month = aug,

day = "26",

doi = "10.1109/ChiCC.2016.7553691",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "2176--2181",

editor = "Jie Chen and Qianchuan Zhao and Jie Chen",

booktitle = "Proceedings of the 35th Chinese Control Conference, CCC 2016",

address = "美国",

}

Duan, G, Huang, X & Xu, G 2016, Parameter identification of spacecraft rendezvous under non-cooperative case. in J Chen, Q Zhao & J Chen (eds), Proceedings of the 35th Chinese Control Conference, CCC 2016., 7553691, Chinese Control Conference, CCC, vol. 2016-August, IEEE Computer Society, pp. 2176-2181, 35th Chinese Control Conference, CCC 2016, Chengdu, China, 27/07/16. https://doi.org/10.1109/ChiCC.2016.7553691

Parameter identification of spacecraft rendezvous under non-cooperative case. / Duan, Guangren; Huang, Xiuwei; Xu, Gang.
Proceedings of the 35th Chinese Control Conference, CCC 2016. ed. / Jie Chen; Qianchuan Zhao; Jie Chen. IEEE Computer Society, 2016. p. 2176-2181 7553691 (Chinese Control Conference, CCC; Vol. 2016-August).

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

TY - GEN

T1 - Parameter identification of spacecraft rendezvous under non-cooperative case

AU - Duan, Guangren

AU - Huang, Xiuwei

AU - Xu, Gang

PY - 2016/8/26

Y1 - 2016/8/26

N2 - In this paper, the problem about parameter identification of spacecraft rendezvous under non-cooperative case is investigated. A new kind of identification method about continuous linear system is proposed. Firstly, linear transform algorithm and generalized bilinear transform algorithm as new discretization algorithms of continuous system are stated. According to these two algorithms, the parameters of continuous and discrete system can be connected by analytical way rather than approximate method, besides, their relationship is reversible. Then, by employing the MIMO recursive extended least squares algorithm, the spacecraft rendezvous system is identified. The simulation results show that the statistic errors of parameter following by two algorithms both converge to zero with the increase of the iteration steps and the latter algorithm has smaller parameter error.

AB - In this paper, the problem about parameter identification of spacecraft rendezvous under non-cooperative case is investigated. A new kind of identification method about continuous linear system is proposed. Firstly, linear transform algorithm and generalized bilinear transform algorithm as new discretization algorithms of continuous system are stated. According to these two algorithms, the parameters of continuous and discrete system can be connected by analytical way rather than approximate method, besides, their relationship is reversible. Then, by employing the MIMO recursive extended least squares algorithm, the spacecraft rendezvous system is identified. The simulation results show that the statistic errors of parameter following by two algorithms both converge to zero with the increase of the iteration steps and the latter algorithm has smaller parameter error.

KW - C-W equation

KW - Discretization algorithm

KW - Non-cooperation

KW - Parameter identification

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DO - 10.1109/ChiCC.2016.7553691

M3 - 会议稿件

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EP - 2181

BT - Proceedings of the 35th Chinese Control Conference, CCC 2016

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A2 - Zhao, Qianchuan

A2 - Chen, Jie

PB - IEEE Computer Society

T2 - 35th Chinese Control Conference, CCC 2016

Y2 - 27 July 2016 through 29 July 2016

ER -

Parameter identification of spacecraft rendezvous under non-cooperative case

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