Multiple Angle Impact Guidance Law Design for Hypersonic Guided Rockets

被引：0

作者：

Li, Jinping ^{[1
]}

Mao, Zhaoyong ^{[2
]}

Li, Yajun ^{[1
]}

Chang, Guannan ^{[1
]}

机构：

[1] Xian Modern Control Technol Res Inst, Xian 710065, Peoples R China

[2] Northwestern Polytech Univ, Xian 710069, Peoples R China

来源：

PROCEEDINGS OF 2022 INTERNATIONAL CONFERENCE ON AUTONOMOUS UNMANNED SYSTEMS, ICAUS 2022 | 2023年 / 1010卷

关键词：

Hypersonic rockets; Multiple angle impact; Impact angle constraint; Implementation approach;

D O I：

10.1007/978-981-99-0479-2_123

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

To Guarantee the warhead effectiveness, it usually requires that the hypersonic guided rocket attacks the target with a designated and sufficient large impact angle. To address such problem, a new multiple angle impact guidance law is proposed in this paper. Firstly, the design process of the proposed guidance law with impact angle constraint is presented. Then, the implementation approach of the developed guidance law is analyzed. Finally, the correctness and validity of the guidance law are verified by the simulation of the closed-loop 6-dof model.

引用

页码：1349 / 1355

页数：7

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