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Dynamic stability of rolling missiles with angle-of-attack feedback three-loop autopilot considering parasitic effect

Dynamic stability of rolling missiles with angle-of-attack feedback three-loop autopilot considering parasitic effect

Tian, Song; Lin, Defu; Wang, Jiang; Li, Bin

期刊名称Aerospace Science and Technology
作者Tian, Song; Lin, Defu; Wang, Jiang; Li, Bin
印刷ISSN1270-9638
文件大小1282.41KB
发表时间2017-10
DOI10.1016/j.ast.2017.10.023

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