计算机测量与控制2024,Vol.32Issue(5) :24-30.DOI:10.16526/j.cnki.11-4762/tp.2024.05.004

基于光电标签的火箭橇全程测速技术研究

Research on Rocket Sled Full-range Velocity Measurement Technology Based on Optoelectronic Tags

李翰宗 蔡荣立 侯丹妮
计算机测量与控制2024,Vol.32Issue(5) :24-30.DOI:10.16526/j.cnki.11-4762/tp.2024.05.004

基于光电标签的火箭橇全程测速技术研究

Research on Rocket Sled Full-range Velocity Measurement Technology Based on Optoelectronic Tags

李翰宗 1蔡荣立 1侯丹妮1
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作者信息

  • 1. 西安工业大学光电工程学院,西安 710021
  • 折叠

摘要

火箭橇试验在兵器研制和性能测试上起着至关重要的作用,现有火箭橇测速方法均存在一些不足之处,针对火箭橇试验中全程速度测量难题,提出了一种基于光电标签的火箭橇全程速度测量方法;建立了光电标签的探测模型,对光电标签的原向反射特性进行研究,分析并仿真了传感器在动态测量中的信号变化过程,基于信号的频率特性对光电探测器件与信号处理电路进行选型,设计并搭建出硬件测量电路,对系统进行了测试与验证;实验结果表明:传感器对光电标签的探测距离可达40 cm,系统速度测量范围满足了火箭橇试验在兵器靶场上的应用,与传统方法相比,光电标签法成本更低、易实现,在火箭橇全程速度测量中有更广泛的应用场景.

Abstract

Rocket sled testing plays a crucial role in weapon development and performance evaluation.However,existing meth-ods have some shortcomings for rocket sled velocity measurement.To address the challenge of full-range velocity measurement in rocket sled testing,an optoelectronic tag-based method for full-range velocity measurement is proposed.Establish the detection model for optoelectronic tags,investigate their directional reflection characteristics,analyze and simulate the signal variation process of the sensor during dynamic measurements,select the photoelectric detection device based on the frequency characteristics of the signal,build the hardware measurement circuits,and validate the system.Experimental results demonstrate that the detect distance of the sensor to the photoelectric tags reaches up to 40 cm,and the velocity measurement range meets the requirements for rocket sled tes-ting at weapon proving grounds.Compared to traditional methods,the optoelectronic tag method has lower cost and broader applica-bility in full-range velocity measurement for rocket sleds.

关键词

火箭橇试验/光电标签/FPGA/光电探测/速度测量

Key words

rocket sled testing/photoelectric tags/FPGA/photoelectric detection/velocity measurement

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出版年

2024
计算机测量与控制
中国计算机自动测量与控制技术协会

计算机测量与控制

CSTPCD
影响因子:0.546
ISSN:1671-4598
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