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弹载单脉冲探测器前视测高策略研究
引用本文:程呈,高敏,周晓东,柯知非,惠江海. 弹载单脉冲探测器前视测高策略研究[J]. 兵工学报, 2019, 40(9): 1819-1828. DOI: 10.3969/j.issn.1000-1093.2019.09.007
作者姓名:程呈  高敏  周晓东  柯知非  惠江海
作者单位:陆军工程大学石家庄校区导弹工程系,河北石家庄,050003;陆军工程大学石家庄校区弹药工程系,河北石家庄,050003
基金项目:武器装备“十三五”预先研究项目(30107030803)
摘    要:新型炸高可选择近炸引信需要实时获取载弹对地高程,用以实施预设作战任务。提出一种弹载单脉冲探测器前视测高策略,在实时性要求较高的弹载平台实现了对地高程的高精度、快速解算。建立弹载探测器测高模型,从单脉冲测距理论出发,推导得到弹载单脉冲探测器的测高算法,并通过仿真以及外场试验对该算法进行验证。结果表明:单脉冲测高体制能够满足新型炸高可选择近炸引信对于炸高的精度要求,仿真测高平均误差为7.8%;挂飞试验测高误差不超过2.5 m,整体响应耗时能够满足弹载平台需求。

关 键 词:远程制导火箭弹  弹载探测器  单脉冲  测高策略
收稿时间:2018-11-21

Research on Looking-forward Altimetry Strategy for Missile-borne Monopulse Detector
CHENG Cheng,GAO Min,ZHOU Xiaodong,KE Zhifei,HUI Jianghai. Research on Looking-forward Altimetry Strategy for Missile-borne Monopulse Detector[J]. Acta Armamentarii, 2019, 40(9): 1819-1828. DOI: 10.3969/j.issn.1000-1093.2019.09.007
Authors:CHENG Cheng  GAO Min  ZHOU Xiaodong  KE Zhifei  HUI Jianghai
Affiliation:(1.Department of Missile Engineering,Shijiazhuang Campus, Army Engineering University, Shijiazhuang 050003, Hebei, China;2.Department of Ammunition Engineering,Shijiazhuang Campus, Army Engineering University, Shijiazhuang 050003, Hebei, China)
Abstract:The height of missile needs to be acquired in real time to perform the preset combat missions for the new generation optional burst height proximity fuze. A forward-looking altimetry strategy for missile-borne monopulse detector is proposed, which achieves high precision and fast terrain elevation calculation on the missile-borne platform with high real-time requirements. An altimetry model of missile-borne detector is established, and the altimetry algorithm of missile-borne monopulse detector is deduced from the theory of monopulse ranging. The altimetry algorithm is verified by simulation and field test. The experimental results show that the monopulse altimetry system can meet the precision requirement of the new optional burst height proximity fuze for burst height. The average error of simulation altimetry is 7.8%, the altimetry error of suspension flight test is less than 2.5 m, and the overall response time can meet the needs of the missile-borne platform.
Keywords:long-range guided rocket   missile-borne detector   monopulse   altimeter strategy  
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