| 一种划定反舰导弹飞行航区的方法研究 |
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| 引用本文： | 李永胜,许诚,王伟力,乔勇军. 一种划定反舰导弹飞行航区的方法研究[J]. 飞行力学, 2009, 27(1) |
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| 作者姓名： | 李永胜 许诚 王伟力 乔勇军 |
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| 作者单位： | 1. 海军航空工程学院,兵器科学与技术系,山东,烟台,264001
2. 海军航空工程学院,飞行器工程系,山东,烟台,264001 |
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| 摘 要： | 考虑到反舰导弹试验与训练的安全性,引入反舰导弹飞行航区的定义.探讨了4个影响飞行航区划定因素:舰面干扰、风干扰、陀螺漂移干扰、导弹故障干扰,构建了反舰导弹干扰作用下的全弹道模型.进而以设定的导弹参数为例,划定飞行航区,通过与实际靶试对照,验证了该方案的合理性与优越性.
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| 关 键 词： | 反舰导弹 飞行航区 弹道模型 仿真 |
Research on the Design about Flight Test Region of Anti-Ship Missile |
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| LI Yong-sheng,XU Cheng,WANG Wei-li,QIAO Yong-jun. Research on the Design about Flight Test Region of Anti-Ship Missile[J]. Flight Dynamics, 2009, 27(1) |
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| Authors: | LI Yong-sheng XU Cheng WANG Wei-li QIAO Yong-jun |
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| Affiliation: | 1.Department of Ordnance Science and Technology;NAEI;Yantai 264001;China;2.Department of Aircraft Engineering;China |
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| Abstract: | Considering the safety of anti-ship testing and training,this paper introduced the concept of flight test region,and studied the four factors which affect the design of flight test region,which are ship-deck interference,wind interference,gyro drift interference,fault interference.It constructed the anti-ship whole trajectory model with interferences,then designed the flight test region by setting missile parameters,contrasted the simulation test with the actual range test,and verified the rationality and s... |
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| Keywords: | anti-ship missile flight test region trajectory model simulation |
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