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某型教学机载导弹发控系统设计
引用本文:马登武,马羚,吕晓峰,董大为.某型教学机载导弹发控系统设计[J].实验室研究与探索,2011,30(12):52-55.
作者姓名:马登武  马羚  吕晓峰  董大为
作者单位:1. 海军航空工程学院兵器科学与技术系
2. 海军航空工程学院研究生管理大队,山东烟台,264001
3. 92154部队导弹技术队,山东烟台,264001
摘    要:根据机载导弹发控系统的组成和功能,运用计算机仿真技术和虚拟仪器技术,设计了某型教学机载导弹发控系统,给出了系统软、硬件设计方案,对发控逻辑算法、核心硬件功能电路和实时数据收发等关键问题进行了研究.实际使用表明,该系统能够模拟机栽导弹发控系统的所有功能,可用于机栽导弹发控系统实验教学.

关 键 词:实验教学  导弹发控系统  计算机仿真  虚拟仪器

Design of a Teaching Missile Launch Control System
MA Deng-wu , MA Ling , LV Xiao-feng , DONG Da-wei.Design of a Teaching Missile Launch Control System[J].Laboratory Research and Exploration,2011,30(12):52-55.
Authors:MA Deng-wu  MA Ling  LV Xiao-feng  DONG Da-wei
Institution:1a.Department of Ordnance Science and Technology,1b.Administrant Brigade of Postgraduate, Naval Aeronautical and Astronautical University,Yantai 264001,China; 2.Brigade of Missile Technique,PLA No.92154 Troops,Yantai 264001,China)
Abstract:According to the composition and function of missile launch control system,the teaching missile launch control system of a certain fighter was designed by computer simulation and virtual instrument technique.The software and hardware of the teaching system were presented.Some difficult problems were researched,such as the logical arithmetic of missile launch control,the core circuit of hardware and real time data receiving and sending etc.Actual application demonstrates that the design can realize all functions of the missile launch control system and it can be used in the experimental teaching of missile launch control system.
Keywords:experimental teaching  missile launch control system  computer simulation  virtual instrument
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