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歼击机武器火控系统性能试飞评定系统的分析与设计
引用本文:张耀中,张安,何建华. 歼击机武器火控系统性能试飞评定系统的分析与设计[J]. 系统仿真学报, 2003, 15(10): 1467-1470
作者姓名:张耀中  张安  何建华
作者单位:西北工业大学电子工程系,西安,710072
摘    要:火控性能试飞是对机载火控系统的好坏进行评定的重要手段。本文以某型歼击机为对象,给出了火控试飞评定系统的总体设计结构,各分系统的详细设计与实现,同时开发了试飞评定系统的软硬件,并应用于某型战斗机的试飞评定中,证明该评定系统正确可行。

关 键 词:火控系统 性能试飞 CEP(圆概率偏差) 误差传递
文章编号:1004-731X(2003)10-1467-04
修稿时间:2002-10-17

Analysis and Design on Performance Flight-test Assessment System of Fighter''s Fire Control System
ZHANG Yao-zhong,ZHANG An,HE Jian-hua. Analysis and Design on Performance Flight-test Assessment System of Fighter''s Fire Control System[J]. Journal of System Simulation, 2003, 15(10): 1467-1470
Authors:ZHANG Yao-zhong  ZHANG An  HE Jian-hua
Abstract:Performance flight-test of fire control system is an important method to assess the performance of fighters fire control system. As an example, the unitary design frame, the detailed design and implementation of a certain fighter are given, and the software and hardware about the flight-test assess system are also developed. It has been applied to a certain airplane and has been proved to be highly effective.
Keywords:fire control system  performance flight-test  circular error probability  transfer of error
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