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Shuangxi LIU, Binbin YAN, Wei HUANG, Xu ZHANG, Jie YAN. Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review[J]. Journal of Zhejiang University Science A, 1998, -1(-1): .
@article{title="Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review",
author="Shuangxi LIU, Binbin YAN, Wei HUANG, Xu ZHANG, Jie YAN",
journal="Journal of Zhejiang University Science A",
volume="-1",
number="-1",
pages="",
year="1998",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A2200423"
}
%0 Journal Article
%T Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review
%A Shuangxi LIU
%A Binbin YAN
%A Wei HUANG
%A Xu ZHANG
%A Jie YAN
%J Journal of Zhejiang University SCIENCE A
%V -1
%N -1
%P
%@ 1673-565X
%D 1998
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A2200423
TY - JOUR
T1 - Current status and prospects of terminal guidance laws for intercepting hypersonic vehicles in near space: a review
A1 - Shuangxi LIU
A1 - Binbin YAN
A1 - Wei HUANG
A1 - Xu ZHANG
A1 - Jie YAN
J0 - Journal of Zhejiang University Science A
VL - -1
IS - -1
SP -
EP -
%@ 1673-565X
Y1 - 1998
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A2200423
Abstract: The unique performance advantages of hypersonic vehicles represent a critical challenge for existing defense systems. To facilitate defensive operations against hypersonic vehicles in near space, this paper systematically discusses both the advantages of these vehicles and the difficulties in intercepting them. Focusing on the state-of-the-art terminal guidance laws for intercepting hypersonic vehicles in near space, we examine research progress in the area of single- and multi-interceptor cooperative guidance laws and summarize their advantages and disadvantages. We also highlight future research directions for developing an effective terminal guidance law for multi-interceptor cooperative interception of hypersonic vehicles, based on four aspects: the information domain, space domain, physical domain, and effect-cost ratio. The findings provide a reference for further research into near-space interceptor terminal guidance technologies.
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