Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target

Dong Guo; Zixuan Liang; Qingdong Li; Zhang Ren

doi:10.1109/GNCC42960.2018.9018874

Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target

Dong Guo, Zixuan Liang, Qingdong Li, Zhang Ren

Beihang University

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

Abstract

This paper presents a terminal attack area (TAA) calculating method based on analytical geometry for intercepting hypersonic cruise aircraft. Firstly, the missile-target planer relative motion model is established, and the intercepting strategy based on analytic geometry is illustrated. Secondly, the intercept geometry models under non-maneuvering and maneuvering target with minimum or maximum initial lead angles are established. Then, based on the intercept geometry models, the analytic solution formulas for calculating the initial feasible attack area are given. Finally, simulation results indicate that the proposed calculation method based on analytical geometry is more accurate and effective than the traditional numerical calculation method.

Original language	English
Title of host publication	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781538611715
DOIs	https://doi.org/10.1109/GNCC42960.2018.9018874
Publication status	Published - Aug 2018
Externally published	Yes
Event	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 - Xiamen, China Duration: 10 Aug 2018 → 12 Aug 2018

Publication series

Name	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

Conference

Conference	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Country/Territory	China
City	Xiamen
Period	10/08/18 → 12/08/18

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10.1109/GNCC42960.2018.9018874

Cite this

Guo, D., Liang, Z., Li, Q., & Ren, Z. (2018). Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target. In 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 Article 9018874 (2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/GNCC42960.2018.9018874

@inproceedings{ac23177fca55467f9361c5eef663616d,

title = "Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target",

abstract = "This paper presents a terminal attack area (TAA) calculating method based on analytical geometry for intercepting hypersonic cruise aircraft. Firstly, the missile-target planer relative motion model is established, and the intercepting strategy based on analytic geometry is illustrated. Secondly, the intercept geometry models under non-maneuvering and maneuvering target with minimum or maximum initial lead angles are established. Then, based on the intercept geometry models, the analytic solution formulas for calculating the initial feasible attack area are given. Finally, simulation results indicate that the proposed calculation method based on analytical geometry is more accurate and effective than the traditional numerical calculation method.",

author = "Dong Guo and Zixuan Liang and Qingdong Li and Zhang Ren",

note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 ; Conference date: 10-08-2018 Through 12-08-2018",

year = "2018",

month = aug,

doi = "10.1109/GNCC42960.2018.9018874",

language = "English",

series = "2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018",

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

booktitle = "2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018",

address = "United States",

}

Guo, D, Liang, Z, Li, Q & Ren, Z 2018, Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target. in 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018., 9018874, 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018, Institute of Electrical and Electronics Engineers Inc., 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018, Xiamen, China, 10/08/18. https://doi.org/10.1109/GNCC42960.2018.9018874

Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target. / Guo, Dong; Liang, Zixuan; Li, Qingdong et al.
2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018. Institute of Electrical and Electronics Engineers Inc., 2018. 9018874 (2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018).

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

TY - GEN

T1 - Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target

AU - Guo, Dong

AU - Liang, Zixuan

AU - Li, Qingdong

AU - Ren, Zhang

PY - 2018/8

Y1 - 2018/8

N2 - This paper presents a terminal attack area (TAA) calculating method based on analytical geometry for intercepting hypersonic cruise aircraft. Firstly, the missile-target planer relative motion model is established, and the intercepting strategy based on analytic geometry is illustrated. Secondly, the intercept geometry models under non-maneuvering and maneuvering target with minimum or maximum initial lead angles are established. Then, based on the intercept geometry models, the analytic solution formulas for calculating the initial feasible attack area are given. Finally, simulation results indicate that the proposed calculation method based on analytical geometry is more accurate and effective than the traditional numerical calculation method.

AB - This paper presents a terminal attack area (TAA) calculating method based on analytical geometry for intercepting hypersonic cruise aircraft. Firstly, the missile-target planer relative motion model is established, and the intercepting strategy based on analytic geometry is illustrated. Secondly, the intercept geometry models under non-maneuvering and maneuvering target with minimum or maximum initial lead angles are established. Then, based on the intercept geometry models, the analytic solution formulas for calculating the initial feasible attack area are given. Finally, simulation results indicate that the proposed calculation method based on analytical geometry is more accurate and effective than the traditional numerical calculation method.

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U2 - 10.1109/GNCC42960.2018.9018874

DO - 10.1109/GNCC42960.2018.9018874

M3 - Conference contribution

AN - SCOPUS:85082438987

T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

Y2 - 10 August 2018 through 12 August 2018

ER -

Guo D, Liang Z, Li Q, Ren Z. Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target. In 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018. Institute of Electrical and Electronics Engineers Inc. 2018. 9018874. (2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018). doi: 10.1109/GNCC42960.2018.9018874

Analytical geometry-based terminal attack area calculation method for intercepting hypersonic cruise target

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