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

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Institute of Technology

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

1 Citation (Scopus)

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.

Original language	English
Title of host publication	Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
Pages	2769-2772
Number of pages	4
DOIs	https://doi.org/10.1109/EMEIT.2011.6023676
Publication status	Published - 2011
Event	2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 - Harbin, China Duration: 12 Aug 2011 → 14 Aug 2011

Publication series

Name	Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
Volume	6

Conference

Conference	2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011
Country/Territory	China
City	Harbin
Period	12/08/11 → 14/08/11

Keywords

Modeling
Transitional ballistic trajectory
optimization

Access to Document

10.1109/EMEIT.2011.6023676

Cite this

Ma, W., Song, X., & Yao, X. (2011). Transitional ballistic trajectory optimization of a supersonic target cruise missile. In Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011 (pp. 2769-2772). Article 6023676 (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011; Vol. 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. pp. 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. in 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, vol. 6, pp. 2769-2772, 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011, Harbin, China, 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. p. 2769-2772 6023676 (Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011; Vol. 6).

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

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AU - Song, Xiaodong

AU - Yao, Xiaoxian

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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.

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KW - Transitional ballistic trajectory

KW - optimization

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Ma W, Song X, Yao X. Transitional ballistic trajectory optimization of a supersonic target cruise missile. In Proceedings of 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011. 2011. p. 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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