Suboptimal Midcourse Guidance with Terminal-Angle Constraint for Hypersonic Target Interception

For the problem of hypersonic target interception, a novel midcourse guidance method with terminal-angle constraint is proposed. Referring to the air-breathing and the boost-gliding hypersonic targets, flight characteristics and difficulties of interception are analyzed, respectively. The requiremen...

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Bibliographic Details
Main Authors: Shizheng Wan, Xiaofei Chang, Quancheng Li, Jie Yan
Format: Article
Language:English
Published: Wiley 2019-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2019/6161032
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