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Extended differential geometric guidance law for intercepting maneuvering targets 被引量:4
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作者 HUANG Jingshuai ZHANG Hongbo +1 位作者 TANG Guojian BAO Weimin 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2018年第5期1046-1057,共12页
Without assumptions made on motion states of missile and target, an extended differential geometric guidance law is derived. Through introducing a line of sight rotation coordinate system, the derivation is simplified... Without assumptions made on motion states of missile and target, an extended differential geometric guidance law is derived. Through introducing a line of sight rotation coordinate system, the derivation is simplified and has more explicit physical significances. The extended law is theoretically applicable to any engagement scenarios. Then, on basis of the extended law, a modified one is designed without the requirement of target acceleration and an approach is proposed to determining the applied direction of commanded missile acceleration. Qualitative analysis is carried out to study the capture performance and a criterion for capture is given. Simulation results indicate the two laws are effective and make up the deficiency that pure proportional navigation suitable for endoatmospheric interceptions cannot deal with high-speed maneuvering targets. Furthermore, the correctness of the criterion is validated. 展开更多
关键词 missile guidance maneuvering target extended differential geometric guidance law capture performance proportional navigation
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