导弹轨上参数测量的技术实现  

Technical Realization of Measuring Missile's Orbital parameter

作　　者：张建军[1] 焦淑瑜[1] 张戈[1] 

机构地区：[1]92941部队93分队

出　　处：《计算机测量与控制》2007年第11期1564-1565,1577,共3页Computer Measurement &Control

摘　　要：介绍了一种利用光电探测器、玻璃微珠原向反射片和数字存储器等高新技术,实现了导弹在发射筒中运动的位移-时间曲线和速度-时间曲线,并由此获得导弹的弹动时刻、离轨时刻和出筒时刻;阐述了功能结构和基于VC平台下的软硬件的实现过程,实验结果表明,该测量系统运行稳定可靠,测量精度高,解决了在大冲力、强温环境下的数据录取工作,对确保导弹轨上参数的有效录取起到了至关重要的作用。Introducing a new high technology, the technology uses photoelectricity detector bar and glass micro-dew literal direction reflection piece and digital memory to realize the displacement-time curve and the speed-time curve when the missile is moving in the launcher, As a result, we can get the starting-time, the orbit-leaving time and the out of launcher time of the missile. Its structure and the de sign and realization of the hardware and software based on Vc plateform are discussed. The practical operation shows that the system has the advantage of stability, high-speed and precision. This technology solves the data operating under the condition of impulsive force and strength temperature, it has very important function for getting the missile orbital parameter effectively.

关 键 词：探测器 反射片 存储器 

分 类 号：TP274[自动化与计算机技术—检测技术与自动化装置] TJ76[自动化与计算机技术—控制科学与工程]