Variable centroid control scheme over hypersonic tactical missile

易彦; 周凤岐

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Variable centroid control scheme over hypersonic tactical missile

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摘要

This paper presents a brand-new tactical missile control scheme--variable centroid vector control according to the international highlight in the field of missile control and the research status of hypersonic missile control in China. Four critical problems related with the new control method are included: improving phase control in the spinning missile single-channel control; establishing variable centroid controlled spinning missile attitude dynamics equations; analyzing variable centroid control strategies and analyzing the stability of the controlled missile and implementing robust control. The achievements and results obtained are valuable and helpful to the theoretical explorations and engineering applications.

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《中国科学:物理学力学天文学（英文版）》 |2003年第6期|561-569|共9页
作者
易彦; 周凤岐;
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作者单位

Institute of Image Communication and Information Processing Shanghai Jiaotong University Shanghai 200030 China;

College of Aeronautics Northwestern Polytechnical University Xi'an 710072 China;

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原文格式 PDF
正文语种 chi
中图分类物理学;
关键词
hypersonic spinning tactical missile; phase control; variable centroid vector control; stability analysis;

机译：超音速纺纱战术导弹;相控;可变质心矢量控制;稳定性分析;

Variable centroid control scheme over hypersonic tactical missile

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