Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach

Binglong Cong; Xiangdong Liu; Zhen Chen

doi:10.1109/ICEICE.2011.5778361

Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach

Binglong Cong^*, Xiangdong Liu, Zhen Chen

^*Corresponding author for this work

School of Automation

Beijing Institute of Technology

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

Abstract

In this paper, the attitude tracking problem of rigid spacecraft without inertial or relative angular velocity measurements is investigated. The minimal attitude description, the modified Rodrigues parameters (MRPs), are utilized as the attitude parameters for the non-redundancy. The inherent passivity of the system describing the attitude tracking motion of the spacecraft is exploited. Then an attitude tracking control law using feedback parts of relative angular velocity and relative MRPs is designed. Additionally, to remove the requirement of the relative angular velocity measurements, a lead filter is utilized to provide the information for the tracking control problem with relative attitude measurements only. Finally, a numerical simulation is employed to verify the proposed control algorithm.

Original language	English
Title of host publication	2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings
Pages	196-201
Number of pages	6
DOIs	https://doi.org/10.1109/ICEICE.2011.5778361
Publication status	Published - 2011
Event	2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Wuhan, China Duration: 15 Apr 2011 → 17 Apr 2011

Publication series

Name	2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings

Conference

Conference	2011 International Conference on Electric Information and Control Engineering, ICEICE 2011
Country/Territory	China
City	Wuhan
Period	15/04/11 → 17/04/11

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10.1109/ICEICE.2011.5778361

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Cong, B., Liu, X., & Chen, Z. (2011). Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach. In 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings (pp. 196-201). Article 5778361 (2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings). https://doi.org/10.1109/ICEICE.2011.5778361

Cong, Binglong ; Liu, Xiangdong ; Chen, Zhen. / Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach. 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings. 2011. pp. 196-201 (2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings).

@inproceedings{8967b83c10c44a53bb94746b19e0782a,

title = "Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach",

abstract = "In this paper, the attitude tracking problem of rigid spacecraft without inertial or relative angular velocity measurements is investigated. The minimal attitude description, the modified Rodrigues parameters (MRPs), are utilized as the attitude parameters for the non-redundancy. The inherent passivity of the system describing the attitude tracking motion of the spacecraft is exploited. Then an attitude tracking control law using feedback parts of relative angular velocity and relative MRPs is designed. Additionally, to remove the requirement of the relative angular velocity measurements, a lead filter is utilized to provide the information for the tracking control problem with relative attitude measurements only. Finally, a numerical simulation is employed to verify the proposed control algorithm.",

author = "Binglong Cong and Xiangdong Liu and Zhen Chen",

year = "2011",

doi = "10.1109/ICEICE.2011.5778361",

language = "English",

isbn = "9781424480395",

series = "2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings",

pages = "196--201",

booktitle = "2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings",

note = "2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 ; Conference date: 15-04-2011 Through 17-04-2011",

}

Cong, B, Liu, X & Chen, Z 2011, Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach. in 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings., 5778361, 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings, pp. 196-201, 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, Wuhan, China, 15/04/11. https://doi.org/10.1109/ICEICE.2011.5778361

Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach. / Cong, Binglong; Liu, Xiangdong ; Chen, Zhen.
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings. 2011. p. 196-201 5778361 (2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings).

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

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AU - Liu, Xiangdong

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N2 - In this paper, the attitude tracking problem of rigid spacecraft without inertial or relative angular velocity measurements is investigated. The minimal attitude description, the modified Rodrigues parameters (MRPs), are utilized as the attitude parameters for the non-redundancy. The inherent passivity of the system describing the attitude tracking motion of the spacecraft is exploited. Then an attitude tracking control law using feedback parts of relative angular velocity and relative MRPs is designed. Additionally, to remove the requirement of the relative angular velocity measurements, a lead filter is utilized to provide the information for the tracking control problem with relative attitude measurements only. Finally, a numerical simulation is employed to verify the proposed control algorithm.

AB - In this paper, the attitude tracking problem of rigid spacecraft without inertial or relative angular velocity measurements is investigated. The minimal attitude description, the modified Rodrigues parameters (MRPs), are utilized as the attitude parameters for the non-redundancy. The inherent passivity of the system describing the attitude tracking motion of the spacecraft is exploited. Then an attitude tracking control law using feedback parts of relative angular velocity and relative MRPs is designed. Additionally, to remove the requirement of the relative angular velocity measurements, a lead filter is utilized to provide the information for the tracking control problem with relative attitude measurements only. Finally, a numerical simulation is employed to verify the proposed control algorithm.

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DO - 10.1109/ICEICE.2011.5778361

M3 - Conference contribution

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SN - 9781424480395

T3 - 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings

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BT - 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings

T2 - 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011

Y2 - 15 April 2011 through 17 April 2011

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Cong B, Liu X , Chen Z. Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach. In 2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings. 2011. p. 196-201. 5778361. (2011 International Conference on Electric Information and Control Engineering, ICEICE 2011 - Proceedings). doi: 10.1109/ICEICE.2011.5778361

Attitude tracking of rigid spacecraft without angular velocity measurements via passivity approach

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