A sliding mode guidance law with autopilot dynamic lag compensation and attack angle constraint

被引：0
|
作者：
Xu, Shuai [1 ]
Gao, Min [1 ]
Fang, Dan [1 ]
Li, Chaowang [1 ]
Liu, Pu [2 ]
机构：
[1] Army Engineering College, No.97 Heping West Road, Shijiazhuang,Hebei,050003, China
[2] North Institute of Electronic Research, No.2 Zhi Village, Hai Dian District, Beijing,100000, China
来源：
Engineering Letters | 2019年 / 27卷 / 01期
关键词：
Closed loop systems - Backstepping - Air navigation - Sliding mode control;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
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页码：140 / 150
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