Hypersonic vehicle attitude control based on new fast terminal sliding mode

被引：4
|
作者：
Liu, Yuchao [1 ]
Guo, Jianguo [1 ]
Zhou, Jun [1 ]
Wang, Guoqing [2 ]
机构：
[1] Institute for Precise Guidance and Control, Northwestern Polytechnical University, Xi'an,71007, China
[2] Research and Development Center, China Academy of Launch Vehicle Technology, Beijing,100076, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2015年 / 36卷 / 07期
关键词：
Compendex;
D O I：
10.7527/S1000-6893.2014.0290
中图分类号：
学科分类号：
摘要：
Hypersonic vehicles
引用
收藏
页码：2372 / 2380
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