| 飞航导弹飞行包络影响因素分析 |
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| 引用本文： | 何兵,刘刚,雷刚,王圆圆.飞航导弹飞行包络影响因素分析[J].飞行器测控学报,2011(2):84-88. |
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| 作者姓名： | 何兵 刘刚 雷刚 王圆圆 |
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| 作者单位： | 第二炮兵工程学院; |
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| 摘 要： | 飞航导弹飞行包络确定是保障导弹飞行安全的重要基础。本文根据飞航导弹飞行过程,分析了飞行过程中的主要误差,并分别建立了飞航导弹航向和纵向飞行包络的误差模型,确立了各飞行阶段飞行包络半径大小计算方法,为飞航导弹的飞行安全研究提供了基础。
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| 关 键 词： | 飞航导弹 飞行包络 误差分析 |
Research on Factors of Influence on Cruise Missile Flight Envelope |
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| HE Bing,LIU Gang,LEI Gang,WANG Yuanyuan.Research on Factors of Influence on Cruise Missile Flight Envelope[J].Journal of Spacecraft TT&C Technology,2011(2):84-88. |
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| Authors: | HE Bing LIU Gang LEI Gang WANG Yuanyuan |
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| Institution: | HE Bing,LIU Gang,LEI Gang,WANG Yuanyuan(The Second Artillery Engineering College,Xi'an,Shaanxi Province 710025) |
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| Abstract: | The determination of flight envelope of cruise missiles is a key factor for flight safety.The paper analyzes the main flight errors according to the flight course of cruise missiles and establishes a horizontal and vertical flight envelope error model.Equations for computing the radius of flight envelope are also given.The research result is significant for the flight safety of cruise missiles. |
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| Keywords: | Cruise Missile Flight Envelope Error Analysis |
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