Relative attitude determination for fly-around based on UKF

Yongqiang Jin; Xiangdong Liu; Chaozhen Hou

doi:10.1109/WCICA.2008.4593896

Relative attitude determination for fly-around based on UKF

Yongqiang Jin^*, Xiangdong Liu, Chaozhen Hou

^*Corresponding author for this work

School of Automation

Beijing Institute of Technology

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

1 Citation (Scopus)

Abstract

To solve the problem of relative attitude determination of a deputy satellite with respect to chief satellite in fly-around, unscented Kalman filter (UKF) method of relative attitude determination is presented. The minimum representation of the attitude, modified Rodrigues parameter (MRP) is adopted as the attitude representation parameter. Combination of gyro, star tracker and laser rendezvous radar are employed as the attitude sensors. The state equation of relative attitude determination is obtained with consideration of relative attitude dynamic equation. Therefore, the UKF model is constructed. Simulations are done and the comparison with that of extended Kalman filter (EKF) shows that the UKF method has a faster convergence speed and a higher estimation precision.

Original language	English
Title of host publication	Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	6397-6401
Number of pages	5
ISBN (Print)	9781424421145
DOIs	https://doi.org/10.1109/WCICA.2008.4593896
Publication status	Published - 2008
Event	7th World Congress on Intelligent Control and Automation, WCICA'08 - Chongqing, China Duration: 25 Jun 2008 → 27 Jun 2008

Publication series

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

Conference

Conference	7th World Congress on Intelligent Control and Automation, WCICA'08
Country/Territory	China
City	Chongqing
Period	25/06/08 → 27/06/08

Keywords

Fly-around
Laser rendezvous radar
Relative attitude determination
Unscented Kalman filter

Access to Document

10.1109/WCICA.2008.4593896

Cite this

Jin, Y., Liu, X., & Hou, C. (2008). Relative attitude determination for fly-around based on UKF. In Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08 (pp. 6397-6401). Article 4593896 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA)). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/WCICA.2008.4593896

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title = "Relative attitude determination for fly-around based on UKF",

abstract = "To solve the problem of relative attitude determination of a deputy satellite with respect to chief satellite in fly-around, unscented Kalman filter (UKF) method of relative attitude determination is presented. The minimum representation of the attitude, modified Rodrigues parameter (MRP) is adopted as the attitude representation parameter. Combination of gyro, star tracker and laser rendezvous radar are employed as the attitude sensors. The state equation of relative attitude determination is obtained with consideration of relative attitude dynamic equation. Therefore, the UKF model is constructed. Simulations are done and the comparison with that of extended Kalman filter (EKF) shows that the UKF method has a faster convergence speed and a higher estimation precision.",

keywords = "Fly-around, Laser rendezvous radar, Relative attitude determination, Unscented Kalman filter",

author = "Yongqiang Jin and Xiangdong Liu and Chaozhen Hou",

year = "2008",

doi = "10.1109/WCICA.2008.4593896",

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isbn = "9781424421145",

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

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

pages = "6397--6401",

booktitle = "Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08",

address = "United States",

note = "7th World Congress on Intelligent Control and Automation, WCICA'08 ; Conference date: 25-06-2008 Through 27-06-2008",

}

Jin, Y, Liu, X & Hou, C 2008, Relative attitude determination for fly-around based on UKF. in Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08., 4593896, Proceedings of the World Congress on Intelligent Control and Automation (WCICA), Institute of Electrical and Electronics Engineers Inc., pp. 6397-6401, 7th World Congress on Intelligent Control and Automation, WCICA'08, Chongqing, China, 25/06/08. https://doi.org/10.1109/WCICA.2008.4593896

Relative attitude determination for fly-around based on UKF. / Jin, Yongqiang; Liu, Xiangdong; Hou, Chaozhen.
Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08. Institute of Electrical and Electronics Engineers Inc., 2008. p. 6397-6401 4593896 (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 - Relative attitude determination for fly-around based on UKF

AU - Jin, Yongqiang

AU - Liu, Xiangdong

AU - Hou, Chaozhen

PY - 2008

Y1 - 2008

N2 - To solve the problem of relative attitude determination of a deputy satellite with respect to chief satellite in fly-around, unscented Kalman filter (UKF) method of relative attitude determination is presented. The minimum representation of the attitude, modified Rodrigues parameter (MRP) is adopted as the attitude representation parameter. Combination of gyro, star tracker and laser rendezvous radar are employed as the attitude sensors. The state equation of relative attitude determination is obtained with consideration of relative attitude dynamic equation. Therefore, the UKF model is constructed. Simulations are done and the comparison with that of extended Kalman filter (EKF) shows that the UKF method has a faster convergence speed and a higher estimation precision.

AB - To solve the problem of relative attitude determination of a deputy satellite with respect to chief satellite in fly-around, unscented Kalman filter (UKF) method of relative attitude determination is presented. The minimum representation of the attitude, modified Rodrigues parameter (MRP) is adopted as the attitude representation parameter. Combination of gyro, star tracker and laser rendezvous radar are employed as the attitude sensors. The state equation of relative attitude determination is obtained with consideration of relative attitude dynamic equation. Therefore, the UKF model is constructed. Simulations are done and the comparison with that of extended Kalman filter (EKF) shows that the UKF method has a faster convergence speed and a higher estimation precision.

KW - Fly-around

KW - Laser rendezvous radar

KW - Relative attitude determination

KW - Unscented Kalman filter

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M3 - Conference contribution

AN - SCOPUS:52149117674

SN - 9781424421145

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

SP - 6397

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BT - Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08

PB - Institute of Electrical and Electronics Engineers Inc.

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Jin Y, Liu X, Hou C. Relative attitude determination for fly-around based on UKF. In Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08. Institute of Electrical and Electronics Engineers Inc. 2008. p. 6397-6401. 4593896. (Proceedings of the World Congress on Intelligent Control and Automation (WCICA)). doi: 10.1109/WCICA.2008.4593896

Relative attitude determination for fly-around based on UKF

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