基于系统融合性指标设计的飞行数据实时回传系统构建与应用  

Construction and Implementation of Real-time Flight Data Transmission System Based on Fusion Index

作　　者：于守淼 于向阳 姚凌虹 于春风 王赛 YU Shoumiao;YU Xiangyang;YAO Linghong;YU Chunfeng;WANG Sai(Qingdao Campus of Naval Aviation University,Qingdao 266041)

机构地区：[1]海军航空大学青岛校区,青岛266041

出　　处：《舰船电子工程》2020年第9期67-70,共4页Ship Electronic Engineering

基　　金：国防科研事业基金项目“飞机电路控制器件检测与修理通用技术研究”(编号:0610);军内科研项目“飞机线路性能评估技术研究”(编号:425111319)资助。

摘　　要：在定型飞机上加装任务系统,往往因原机交联关系复杂,电磁环境不确定因素多,布线路径受限等实施困难。论文采用综合化集成技术,将电源容量、重量重心、电缆布线、电磁兼容等可靠性因素作为系统融合性指标,构建了某型机基于信息化通讯平台的空中飞行训练实时监控系统,解决了空、地勤人员缺乏机上实时动态数据的难题,投入使用后,工作稳定可靠,对飞机相关系统设计具有一定的技术牵引和借鉴价值。It is often difficult to install the task system on the finalizing aircraft due to the complex relationship between the original aircraft systems,multiple uncertainties in the electromagnetic environment,limited wiring path,etc.Based on the compre⁃hensive integration technology,this paper puts the power capacity,weight,center of gravity,cable wiring reliability,electromagnetic compatibility and other factors as indicators of system integration.Based on the flight training information communication platform,this paper builds a real-time monitoring system which solves the pilots,ground staff on the problem of lack of real-time dynamic da⁃ta on board.After putting it into use,work is stable and reliable,which has a certain technical drawing and reference value related to the aircraft system design.

关 键 词：加装 飞行数据 实时回传 可靠性 电磁兼容 

分 类 号：V243[航空宇航科学与技术—飞行器设计]