Optimal sliding mode servo control with integral term for rocket launcher

被引：0
|
作者：
Zhu, Yu-Chuan [1 ]
Ma, Da-Wei [2 ]
Li, Zhi-Gang [2 ]
Le, Gui-Gao [2 ]
机构：
[1] College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
[2] School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
来源：
Binggong Xuebao/Acta Armamentarii | 2007年 / 28卷 / 10期
关键词：
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页码：1272 / 1275
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