Design of dynamic inversion control systems for missiles based on trajectory linearization

被引：0
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作者：
Yang, Zhi-Feng [1 ]
Lei, Hu-Min [1 ]
Li, Qing-Liang [1 ]
Li, Jiong [1 ]
机构：
[1] The Missile Institute of Air Force Engineering University, Sanyuan 713800, China
来源：
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2011年 / 34卷 / 01期
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