Attitude control design for launch vehicle with appointed performance

被引：0

作者：

Zhang, Liang ^{[1
]}

Li, Danyu ^{[1
]}

Cui, Naigang ^{[2
]}

机构：

[1] School of Aeronautics and Astronautics, Sun Yat-Sen University, Shenzhen,518107, China

[2] School of Astronautics, Harbin Institute of Technology, Harbin,150001, China

来源：

Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology | 2022年 / 30卷 / 06期

关键词：

Compendex;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Launch vehicles

引用

页码：807 / 813