Partial integrated guidance and control method for the interception of nearspace hypersonic target

Bin Fu; Wenxing Fu; Hang Guo; Kang Chen; Xiaofei Chang

doi:10.1109/ICCA.2017.8003100

Partial integrated guidance and control method for the interception of nearspace hypersonic target

Bin Fu, Wenxing Fu, Hang Guo, Kang Chen, Xiaofei Chang

Unmanned System Research Institute

Northwestern Polytechnical University Xian

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

3 Scopus citations

Abstract

The interception of the hypersonic weapons in near space is the main problem considered in this paper. Different from traditional interception cases, the designed interceptor is assumed to have much lower speed than its target and very limited maneuverability in the near space atmosphere. To deal with this problem, a two-loop Partial Integrated Guidance and Control (PIGC) scheme using high order sliding mode control method is introduced in this design. More specifically, an integrated full state feedback guidance loop and an inner state feedback control loop together provide a quick and stable response to the target maneuver. At last numerical simulation results are given to demonstrate the superiority of the proposed method.

Original language	English
Title of host publication	2017 13th IEEE International Conference on Control and Automation, ICCA 2017
Publisher	IEEE Computer Society
Pages	437-442
Number of pages	6
ISBN (Electronic)	9781538626795
DOIs	https://doi.org/10.1109/ICCA.2017.8003100
State	Published - 4 Aug 2017
Event	13th IEEE International Conference on Control and Automation, ICCA 2017 - Ohrid, Macedonia, The Former Yugoslav Republic of Duration: 3 Jul 2017 → 6 Jul 2017

Publication series

Name	IEEE International Conference on Control and Automation, ICCA
ISSN (Print)	1948-3449
ISSN (Electronic)	1948-3457

Conference

Conference	13th IEEE International Conference on Control and Automation, ICCA 2017
Country/Territory	Macedonia, The Former Yugoslav Republic of
City	Ohrid
Period	3/07/17 → 6/07/17

Keywords

arbitrary order robust exact differentiator
high order sliding mode control
Hypersonic target interception
partial integrated guidance and control

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10.1109/ICCA.2017.8003100

Cite this

Fu, B., Fu, W., Guo, H., Chen, K., & Chang, X. (2017). Partial integrated guidance and control method for the interception of nearspace hypersonic target. In 2017 13th IEEE International Conference on Control and Automation, ICCA 2017 (pp. 437-442). Article 8003100 (IEEE International Conference on Control and Automation, ICCA). IEEE Computer Society. https://doi.org/10.1109/ICCA.2017.8003100

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title = "Partial integrated guidance and control method for the interception of nearspace hypersonic target",

abstract = "The interception of the hypersonic weapons in near space is the main problem considered in this paper. Different from traditional interception cases, the designed interceptor is assumed to have much lower speed than its target and very limited maneuverability in the near space atmosphere. To deal with this problem, a two-loop Partial Integrated Guidance and Control (PIGC) scheme using high order sliding mode control method is introduced in this design. More specifically, an integrated full state feedback guidance loop and an inner state feedback control loop together provide a quick and stable response to the target maneuver. At last numerical simulation results are given to demonstrate the superiority of the proposed method.",

keywords = "arbitrary order robust exact differentiator, high order sliding mode control, Hypersonic target interception, partial integrated guidance and control",

author = "Bin Fu and Wenxing Fu and Hang Guo and Kang Chen and Xiaofei Chang",

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doi = "10.1109/ICCA.2017.8003100",

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Fu, B, Fu, W, Guo, H, Chen, K & Chang, X 2017, Partial integrated guidance and control method for the interception of nearspace hypersonic target. in 2017 13th IEEE International Conference on Control and Automation, ICCA 2017., 8003100, IEEE International Conference on Control and Automation, ICCA, IEEE Computer Society, pp. 437-442, 13th IEEE International Conference on Control and Automation, ICCA 2017, Ohrid, Macedonia, The Former Yugoslav Republic of, 3/07/17. https://doi.org/10.1109/ICCA.2017.8003100

Partial integrated guidance and control method for the interception of nearspace hypersonic target. / Fu, Bin; Fu, Wenxing; Guo, Hang et al.
2017 13th IEEE International Conference on Control and Automation, ICCA 2017. IEEE Computer Society, 2017. p. 437-442 8003100 (IEEE International Conference on Control and Automation, ICCA).

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

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T1 - Partial integrated guidance and control method for the interception of nearspace hypersonic target

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AU - Fu, Wenxing

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N2 - The interception of the hypersonic weapons in near space is the main problem considered in this paper. Different from traditional interception cases, the designed interceptor is assumed to have much lower speed than its target and very limited maneuverability in the near space atmosphere. To deal with this problem, a two-loop Partial Integrated Guidance and Control (PIGC) scheme using high order sliding mode control method is introduced in this design. More specifically, an integrated full state feedback guidance loop and an inner state feedback control loop together provide a quick and stable response to the target maneuver. At last numerical simulation results are given to demonstrate the superiority of the proposed method.

AB - The interception of the hypersonic weapons in near space is the main problem considered in this paper. Different from traditional interception cases, the designed interceptor is assumed to have much lower speed than its target and very limited maneuverability in the near space atmosphere. To deal with this problem, a two-loop Partial Integrated Guidance and Control (PIGC) scheme using high order sliding mode control method is introduced in this design. More specifically, an integrated full state feedback guidance loop and an inner state feedback control loop together provide a quick and stable response to the target maneuver. At last numerical simulation results are given to demonstrate the superiority of the proposed method.

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ER -

Partial integrated guidance and control method for the interception of nearspace hypersonic target

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