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Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints 期刊论文
International Journal of Automation and Computing, 2018, 卷号: 15, 期号: 2, 页码: 218-227
作者:  Hui-Bo Zhou;  Jun-Hong Song;  Shen-Min Song
浏览  |  Adobe PDF(1104Kb)  |  收藏  |  浏览/下载:126/39  |  提交时间:2021/02/23
Autopilot  impact angle  nonsingular terminal sliding mode  finite-time convergent  guidance.