| 直接侧向力与气动力复合控制技术综述 |
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| 引用本文： | 魏明英.直接侧向力与气动力复合控制技术综述[J].现代防御技术,2012,40(1):52-54,76. |
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| 作者姓名： | 魏明英 |
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| 作者单位： | 北京电子工程总体研究所,北京,100854 |
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| 摘 要： | 基于直接侧向力与气动力复合控制的高精度快响应制导控制技术是新一代大气层内飞行器精确制导的核心技术,具有强烈的军事需求和广泛的应用背景.直接侧向力/气动力复合控制是指通过导弹侧喷发动机(或喷嘴)所产生的直接侧向力与气动力的共同作用,产生复合力,对导弹进行复合控制,实现大幅度提高导弹快速响应能力和机动能力的控制方式.
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| 关 键 词： | 直接侧向力 复合控制 复合控制模式 |
Summary of Blended Control Technology for Missiles with Lateral Jets and Aerodynamic Surfaces |
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| WEI Ming-ying.Summary of Blended Control Technology for Missiles with Lateral Jets and Aerodynamic Surfaces[J].Modern Defence Technology,2012,40(1):52-54,76. |
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| Authors: | WEI Ming-ying |
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| Institution: | WEI Ming-ying(Beijing Inst.of Electronic System Engineering,Beijing 100854,China) |
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| Abstract: | The high precision quick response guidance and control technology based on the blended control with Lateral Jets and Aerodynamic Surfaces is core technology of the new generation end atmospheric missile,which has a wide and bright application future in military.Lateral Jets/Aerodynamic blended control refers to the control mode in which the side jet engine of missile(or nozzle) cooperates with aerodynamic power to produce a compound force to realize a blended control for missile,which can improve the response speed and mobilization ability of missiles greatly. |
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| Keywords: | lateral jets blended control blended control mode |
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