弹载单脉冲探测器前视测高策略研究

doi:10.3969/j.issn.1000-1093.2019.09.007

兵工学报 ›› 2019, Vol. 40 ›› Issue (9): 1819-1828.doi: 10.3969/j.issn.1000-1093.2019.09.007

弹载单脉冲探测器前视测高策略研究

程呈¹，高敏¹，周晓东²，柯知非¹，惠江海¹

(1.陆军工程大学石家庄校区导弹工程系，河北石家庄 050003；2.陆军工程大学石家庄校区弹药工程系，河北石家庄 050003)

收稿日期:2018-11-21 修回日期:2018-11-21 上线日期:2019-10-31
通讯作者: 周晓东（1976—），男，副教授，博士 E-mail:zxd_oec@sina.com
作者简介:程呈（1991—），男，博士研究生。 E-mail: clarence_oec@sina.com
基金资助:
武器装备“十三五”预先研究项目（30107030803）

Research on Looking-forward Altimetry Strategy for Missile-borne Monopulse Detector

CHENG Cheng¹, GAO Min¹, ZHOU Xiaodong², KE Zhifei¹, HUI Jianghai¹

(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)

Received:2018-11-21 Revised:2018-11-21 Online:2019-10-31

摘要/Abstract

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

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. Key

Key words: long-rangeguidedrocket, missile-bornedetector, monopulse, altimeterstrategy

中图分类号:

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.

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.

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第40卷第9期
2019 年9月兵工学报ACTA
ARMAMENTARIIVol.40No.9Sep. 2019

[1]	程呈，高敏，周晓东，纪永祥，宗竹林. 基于波前编码的弹载相控阵探测器凝视高分辨成像[J]. 兵工学报, 2020, 41(6): 1041-1055.
[2]	程呈，高敏，周晓东，李超旺，于波，刘永鹏. 弹载探测器自适应高分辨前视成像策略研究[J]. 兵工学报, 2019, 40(6): 1121-1129.
[3]	王巍, 崔嵬. 基于确定性模型的比相和差单脉冲雷达角闪烁建模算法[J]. 兵工学报, 2013, 34(10): 1258-1265.

弹载单脉冲探测器前视测高策略研究

Research on Looking-forward Altimetry Strategy for Missile-borne Monopulse Detector

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