Module division method of missile based on requirement-function-structure relation matrix

被引：0
|
作者：
Tian, Kunxiao [1 ]
Su, Hua [1 ,2 ]
Long, Yongsong [3 ]
Yang, Yucheng [1 ]
Gong, Chunlin [1 ,2 ]
机构：
[1] School of Astronautics, Northwestern Polytechnical University, Xi'an,710072, China
[2] Shannxi Aerospace Flight Vehicle Design Key Laboratory, Northwestern Polytechnical University, Xi'an,710072, China
[3] Jiangnan Design Institute of Machinery and Electricity, Guiyang,550009, China
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2024年 / 46卷 / 10期
关键词：
Air to air missiles - Military rockets - Structural analysis;
D O I：
10.12305/j.issn.1001-506X.2024.10.17
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：3398 / 3406
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