| 新一代近距格斗空空导弹机动能力分析 |
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| 引用本文： | 谢永强,李舜,于翠,周须峰.新一代近距格斗空空导弹机动能力分析[J].科学技术与工程,2009,9(15). |
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| 作者姓名： | 谢永强 李舜 于翠 周须峰 |
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| 作者单位： | 中国空空导弹研究院,洛阳,471009 |
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| 摘 要： | 格斗空空导弹的机动能力是全弹设计的核心,是总体设计时需解决的关键问题.首先建立了导弹的动力学模型、运动学模型、推力矢量模型、目标运动模型,通过典型弹道的仿真,确定了导弹的机动能力,即导弹的最大转弯角速率和最大过载值,为导弹总体设计提供依据.
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| 关 键 词： | 转弯角速率 需用过载 目标机动 近距格斗导弹 |
Maneuverable Capability Analysis of Advanced Short-range Dogfight Air to Air Missile |
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| XIE Yong-qiang,LI Shun,YU Cui,ZHOU Xu-feng.Maneuverable Capability Analysis of Advanced Short-range Dogfight Air to Air Missile[J].Science Technology and Engineering,2009,9(15). |
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| Authors: | XIE Yong-qiang LI Shun YU Cui ZHOU Xu-feng |
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| Institution: | China Airborne Missile Academy;Luoyang 471009;P.R.China |
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| Abstract: | The maneuverable capability of air to air missile is the very important problem in the overall design of air to air missile.The missile kinetic model,the missile kinematic model,missile TVC model and the target kinematic model are established.By performing typical ballistic trajectory simulations,the maneuverable capability of short-range dogfight missile is confirmed,including the maximum value of turn angular rate and required overload. The results of the maneuverable capability could provide reference on... |
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| Keywords: | turn angular rate required overload target maneuver dogfight missile |
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