Optimal control design method for missile three-loop autopilot

被引：0
|
作者：
Xu, Wanying [1 ]
Zheng, Yongbin [1 ]
Bai, Shengjian [1 ]
Zhang, Wei [2 ]
机构：
[1] College of Inlelligence Science and Technology, National Universily of Defense Technology, Changsha,410073, China
[2] National Innovation Institute of Defense Technology, Academy of Military Sciences, Beijing,100071, China
来源：
Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology | 2024年 / 46卷 / 06期
关键词：
D O I：
10.11887/j.cn.202406021
中图分类号：
学科分类号：
摘要：
24
引用
收藏
页码：194 / 202
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