典型无人机飞行控制系统HEMP效应研究  

Effect of High Altitude Electromagnetic Pulse on Flight Control System of Typical UAV

作　　者：赵墨[1,2] 吴伟 李进玺[1,2] 程引会 马良[1,2] 郭景海 刘逸飞[1,2] ZHAO Mo;WU Wei;LI Jin-xi;CHENG Yin-hui;MA Liang;GUO Jing-hai;LIU Yi-fei(Northwest Institute of Nuclear Technology,Xi’an 710024,China;State Key Laboratory of Intense Pulsed Radiation Simulation and Effect,Xi’an 710024,China)

机构地区：[1]西北核技术研究所,西安710024 [2]强脉冲辐射环境模拟与效应国家重点实验室,西安710024

出　　处：《现代应用物理》2018年第1期71-74,81,共5页Modern Applied Physics

摘　　要：利用飞行仿真系统、数据采集系统和视景仿真系统开展了地面模拟飞行状态下无人机电子学系统抗高空电磁脉冲效应研究,获取了典型效应现象,分析了薄弱环节,为后续开展其他类型电子学系统的高空电磁脉冲效应研究奠定了技术基础。The effect of high altitude electromagnetic pulse(HEMP)on the electronic system of unmanned aerial vehicle(UAV)was studied under ground based flight simulation,by adopting the flight simulation system,data collection system,and vision simulation system.Several typical effect phenomena were obtained and the weakness was analysized in this research,which lays the technical foundation for the following-up study on other electronics systems subjected to the HEMP.

关 键 词：高空核爆电磁脉冲 电子系统 半实物仿真 

分 类 号：TN79[电子电信—电路与系统]