火力与指挥控制2011，Vol.36Issue(5)：160-163,4.
基于FPGA的火箭参数实时监测系统设计
Design of Real-time Monitoring System Based on FPGA for Rocket Parameters
摘要
Abstract
The tested data can be acquired with traditional storage measurement system for rocket only after the launch. However, we do not know whether the parameters of the rocket are abnormal or not before the launch. The real-time monitoring function is added to the traditional storage measurement system to solve the problem above. The working modes of the system are designed and the method of improving the resistance to interference through setting data value of monitor orders specially is put forward. The process of sampling, frame structuring and the transmitting of monitored data are described at length. The system can compensate the limitations of wireless telemetry system and traditional storage measurement system.关键词
火箭/实时监测/采样编帧/FPGAKey words
rocket/ real-time monitoring/ sampling and frame structuring/ FPGA分类
信息技术与安全科学引用本文复制引用
沈三民,狄宋珍,秦丽,熊继军,张文栋..基于FPGA的火箭参数实时监测系统设计[J].火力与指挥控制,2011,36(5):160-163,4.基金项目
国家自然科学基金(50535030) （50535030）
山西省自然科学基金资助项目(2010011026-2) （2010011026-2）
