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直升机载激光指示器发射末制导炮弹射击效能分析
引用本文:钟宜兴,高正,褚政.直升机载激光指示器发射末制导炮弹射击效能分析[J].南京航空航天大学学报,2004,36(4):433-437.
作者姓名:钟宜兴  高正  褚政
作者单位:1. 南京航空航天大学直升机旋翼动力学重点实验室,南京,210016
2. 炮兵学院南京分院研究生队,南京,211132
摘    要:激光末制导炮弹武器系统是炮兵装备的一种精确制导武器,使用时,通常将激光指示器配置在陆地或舰船上。为了更好地发挥该武器系统的作战效能,需要将激光指示器配置在直升机上,这样就可以对反斜面或陆地无法观察到的目标进行射击。本文根据对直升机振动谱峰随机性的分析结果及末制导炮弹的射击特点,近似认为直升机振动导致的射击误差服从正态分布,确定了直升机机动导致的射击误差属于系统误差,建立了评定直升机载激光指示器保障条件下射击效能的数学模型,并对各种影响射击效能的因素作了分析。

关 键 词:直升机  机载激光指示器  发射  末制导炮弹  射击效能
文章编号:1005-2615(2004)04-0433-05
修稿时间:2003年10月14

Operational Effectiveness Analysis of Firing Terminally Guided Shell by Laser Indicator on Helicopter
ZHONG Yi-xing,GAO Zheng,CHU Zheng.Operational Effectiveness Analysis of Firing Terminally Guided Shell by Laser Indicator on Helicopter[J].Journal of Nanjing University of Aeronautics & Astronautics,2004,36(4):433-437.
Authors:ZHONG Yi-xing  GAO Zheng  CHU Zheng
Institution:ZHONG Yi-xing~1,GAO Zheng~1,CHU Zheng~2
Abstract:The weapon system of terminally guided laser shell is necessary to put the indicator on the helicopter to hit the enemy targets in depth or in the reverse side. By analyzing helicopter random vibration and terminally guided laser shell firing error, that the firing error obeys normal probability is consider. The guided error of the system caused by the helicopter and target moving is determined, the mathematical model for evaluating firing effect under this condition is established and various factors influencing the operational effectiveness are analyzed.
Keywords:laser indicator on helicopter  terminally guided laser  firing effect
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