Attitude control design of missiles with dual control based on model predictive control and active disturbance rejection control

被引：0
|
作者：
Bi, Yong-Tao [1 ]
Wang, Yu-Hang [1 ]
Yao, Yu [2 ]
机构：
[1] Research and Development Center, China Academy of Launch Vehicle Technology, Beijing,100076, China
[2] Control and Simulation Center, Harbin Institute of Technology, Harbin,150080, China
来源：
Yuhang Xuebao/Journal of Astronautics | 2015年 / 36卷 / 12期
关键词：
D O I：
10.3873/j.issn.1000-1328.2015.12.005
中图分类号：
学科分类号：
摘要：
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收藏
页码：1373 / 1383
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