Initial alignment method of the INS for the rotary rocket

Mingjie Dong; Bo Wang; Yan Cui

doi:10.1109/IHMSC.2011.40

Initial alignment method of the INS for the rotary rocket

Mingjie Dong^*
, Bo Wang
, Yan Cui

^*此作品的通讯作者

自动化学院

Beijing Institute of Technology

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

Due to the small size of the INS for the rotary rocket system, a scheme that a FOG and a DTG are used as the angular rate sensor is put forward. With the scheme, the system is finished in the volume of θ190mmX180mm. Using the technology of rotating modulation, the influence of the low-accuracy DTG drifts are weakened. The simulation results show that the alignment error of the attitude angles is less than 0.02° within 280s.

源语言	英语
主期刊名	Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011
页	140-143
页数	4
DOI	https://doi.org/10.1109/IHMSC.2011.40
出版状态	已出版 - 2011
活动	3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011 - Hangzhou, 中国期限: 26 8月 2011 → 27 8月 2011

出版系列

姓名	Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011
卷	1

会议

会议	3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011
国家/地区	中国
市	Hangzhou
时期	26/08/11 → 27/08/11

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10.1109/IHMSC.2011.40

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引用此

Dong, M., Wang, B., & Cui, Y. (2011). Initial alignment method of the INS for the rotary rocket. 在 Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011 (页码 140-143). 文章 6038166 (Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011; 卷 1). https://doi.org/10.1109/IHMSC.2011.40

@inproceedings{cec29dc007334974a5514e5b2b0d7184,

title = "Initial alignment method of the INS for the rotary rocket",

abstract = "Due to the small size of the INS for the rotary rocket system, a scheme that a FOG and a DTG are used as the angular rate sensor is put forward. With the scheme, the system is finished in the volume of θ190mmX180mm. Using the technology of rotating modulation, the influence of the low-accuracy DTG drifts are weakened. The simulation results show that the alignment error of the attitude angles is less than 0.02° within 280s.",

keywords = "DTG, FOG, initial alignment, rotating modulation",

author = "Mingjie Dong and Bo Wang and Yan Cui",

year = "2011",

doi = "10.1109/IHMSC.2011.40",

language = "English",

isbn = "9780769544441",

series = "Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011",

pages = "140--143",

booktitle = "Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011",

note = "3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011 ; Conference date: 26-08-2011 Through 27-08-2011",

}

Dong, M, Wang, B & Cui, Y 2011, Initial alignment method of the INS for the rotary rocket. 在 Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011., 6038166, Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011, 卷 1, 页码 140-143, 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011, Hangzhou, 中国, 26/08/11. https://doi.org/10.1109/IHMSC.2011.40

Initial alignment method of the INS for the rotary rocket. / Dong, Mingjie; Wang, Bo; Cui, Yan.
Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011. 2011. 页码 140-143 6038166 (Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011; 卷 1).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Initial alignment method of the INS for the rotary rocket

AU - Dong, Mingjie

AU - Wang, Bo

AU - Cui, Yan

PY - 2011

Y1 - 2011

N2 - Due to the small size of the INS for the rotary rocket system, a scheme that a FOG and a DTG are used as the angular rate sensor is put forward. With the scheme, the system is finished in the volume of θ190mmX180mm. Using the technology of rotating modulation, the influence of the low-accuracy DTG drifts are weakened. The simulation results show that the alignment error of the attitude angles is less than 0.02° within 280s.

AB - Due to the small size of the INS for the rotary rocket system, a scheme that a FOG and a DTG are used as the angular rate sensor is put forward. With the scheme, the system is finished in the volume of θ190mmX180mm. Using the technology of rotating modulation, the influence of the low-accuracy DTG drifts are weakened. The simulation results show that the alignment error of the attitude angles is less than 0.02° within 280s.

KW - DTG

KW - FOG

KW - initial alignment

KW - rotating modulation

UR - https://www.scopus.com/pages/publications/80054957580

U2 - 10.1109/IHMSC.2011.40

DO - 10.1109/IHMSC.2011.40

M3 - Conference contribution

AN - SCOPUS:80054957580

SN - 9780769544441

T3 - Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011

SP - 140

EP - 143

BT - Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011

T2 - 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011

Y2 - 26 August 2011 through 27 August 2011

ER -

Dong M, Wang B, Cui Y. Initial alignment method of the INS for the rotary rocket. 在 Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011. 2011. 页码 140-143. 6038166. (Proceedings - 2011 3rd International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2011). doi: 10.1109/IHMSC.2011.40

Initial alignment method of the INS for the rotary rocket

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