Orbital guidance method for solid rocket based on improved sequential convex optimization

被引：0
|
作者：
Wang, Hongbo [1 ]
Zhang, Ruonan [1 ]
Liang, Zhuo [1 ]
Lyv, Rui [1 ]
机构：
[1] China Academy of Launch Vehicle Technology, Beijing,100076, China
来源：
Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology | 2021年 / 29卷 / 01期
关键词：
D O I：
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中图分类号：
学科分类号：
摘要：
Convex optimization
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页码：119 / 125
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