Transitional ballistic trajectory optimization of a supersonic target cruise missile

Wuju Ma; Xiaodong Song; Xiaoxian Yao

doi:10.1109/EMEIT.2011.6023676

Transitional ballistic trajectory optimization of a supersonic target cruise missile

Wuju Ma^*
, Xiaodong Song
, Xiaoxian Yao

^*此作品的通讯作者

空天科学与技术学院

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

2 引用（Scopus）

摘要

Supersonic target cruise missile flying at zero is a dynamic practical simulator, which simulates the terminal flight character of anti-ship cruise missile. In order to simulator the flight height of anti-ship cruise missile, the target cruise missile must fly low. The transitional ballistic trajectory of supersonic target cruise missile from high to low is important for flying control. In this study, supersonic target cruise missile is investigated and the controllable particle math model is constituted in order to obtain the optimizing transitional ballistic trajectory. Principle of the minimum of optimum control is used to optimize the transitional ballistic trajectory. The results have an important theoretical value for fight control on transitional ballistic trajectory.

源语言	英语
主期刊名	Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
页	2769-2772
页数	4
DOI	https://doi.org/10.1109/EMEIT.2011.6023676
出版状态	已出版 - 2011
活动	2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 - Harbin, 中国期限: 12 8月 2011 → 14 8月 2011

出版系列

姓名	Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
卷	6

会议

会议	2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
国家/地区	中国
市	Harbin
时期	12/08/11 → 14/08/11

访问文件

10.1109/EMEIT.2011.6023676

其它文件与链接

链接到 Scopus 的出版物

引用此

Ma, W., Song, X., & Yao, X. (2011). Transitional ballistic trajectory optimization of a supersonic target cruise missile. 在 Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 (页码 2769-2772). 文章 6023676 (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011; 卷 6). https://doi.org/10.1109/EMEIT.2011.6023676

Ma, Wuju ; Song, Xiaodong ; Yao, Xiaoxian. / Transitional ballistic trajectory optimization of a supersonic target cruise missile. Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011. 2011. 页码 2769-2772 (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011).

@inproceedings{9620a4cb840b4822a6d64e27ce6a81f4,

title = "Transitional ballistic trajectory optimization of a supersonic target cruise missile",

abstract = "Supersonic target cruise missile flying at zero is a dynamic practical simulator, which simulates the terminal flight character of anti-ship cruise missile. In order to simulator the flight height of anti-ship cruise missile, the target cruise missile must fly low. The transitional ballistic trajectory of supersonic target cruise missile from high to low is important for flying control. In this study, supersonic target cruise missile is investigated and the controllable particle math model is constituted in order to obtain the optimizing transitional ballistic trajectory. Principle of the minimum of optimum control is used to optimize the transitional ballistic trajectory. The results have an important theoretical value for fight control on transitional ballistic trajectory.",

keywords = "Modeling, Transitional ballistic trajectory, optimization",

author = "Wuju Ma and Xiaodong Song and Xiaoxian Yao",

year = "2011",

doi = "10.1109/EMEIT.2011.6023676",

language = "English",

isbn = "9781612840857",

series = "Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011",

pages = "2769--2772",

booktitle = "Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011",

note = "2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 ; Conference date: 12-08-2011 Through 14-08-2011",

}

Ma, W, Song, X & Yao, X 2011, Transitional ballistic trajectory optimization of a supersonic target cruise missile. 在 Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011., 6023676, Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011, 卷 6, 页码 2769-2772, 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011, Harbin, 中国, 12/08/11. https://doi.org/10.1109/EMEIT.2011.6023676

Transitional ballistic trajectory optimization of a supersonic target cruise missile. / Ma, Wuju; Song, Xiaodong; Yao, Xiaoxian.
Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011. 2011. 页码 2769-2772 6023676 (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011; 卷 6).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Transitional ballistic trajectory optimization of a supersonic target cruise missile

AU - Ma, Wuju

AU - Song, Xiaodong

AU - Yao, Xiaoxian

PY - 2011

Y1 - 2011

N2 - Supersonic target cruise missile flying at zero is a dynamic practical simulator, which simulates the terminal flight character of anti-ship cruise missile. In order to simulator the flight height of anti-ship cruise missile, the target cruise missile must fly low. The transitional ballistic trajectory of supersonic target cruise missile from high to low is important for flying control. In this study, supersonic target cruise missile is investigated and the controllable particle math model is constituted in order to obtain the optimizing transitional ballistic trajectory. Principle of the minimum of optimum control is used to optimize the transitional ballistic trajectory. The results have an important theoretical value for fight control on transitional ballistic trajectory.

AB - Supersonic target cruise missile flying at zero is a dynamic practical simulator, which simulates the terminal flight character of anti-ship cruise missile. In order to simulator the flight height of anti-ship cruise missile, the target cruise missile must fly low. The transitional ballistic trajectory of supersonic target cruise missile from high to low is important for flying control. In this study, supersonic target cruise missile is investigated and the controllable particle math model is constituted in order to obtain the optimizing transitional ballistic trajectory. Principle of the minimum of optimum control is used to optimize the transitional ballistic trajectory. The results have an important theoretical value for fight control on transitional ballistic trajectory.

KW - Modeling

KW - Transitional ballistic trajectory

KW - optimization

UR - https://www.scopus.com/pages/publications/80053420259

U2 - 10.1109/EMEIT.2011.6023676

DO - 10.1109/EMEIT.2011.6023676

M3 - Conference contribution

AN - SCOPUS:80053420259

SN - 9781612840857

T3 - Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011

SP - 2769

EP - 2772

BT - Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011

T2 - 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011

Y2 - 12 August 2011 through 14 August 2011

ER -

Ma W, Song X, Yao X. Transitional ballistic trajectory optimization of a supersonic target cruise missile. 在 Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011. 2011. 页码 2769-2772. 6023676. (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011). doi: 10.1109/EMEIT.2011.6023676

Transitional ballistic trajectory optimization of a supersonic target cruise missile

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