民用飞机情景识别系统试飞研究  

Flight Test Research on Situation Recognition System for Civil Aircraft

作　　者：武光 梁远东 李畅 

机构地区：[1]中国商飞民用飞机试飞中心,上海200232

出　　处：《民用飞机设计与研究》2014年第3期44-47,66,共5页Civil Aircraft Design & Research

摘　　要：由于平视显示器(HUD)、视景增强系统(EVS)以及合成视景系统(SVS)优秀的情景显示能力,HUD与EVS、SVS结合使用将显著提高飞行机组情景识别以及态势感知能力。同时,HUD与自动着陆系统结合使用可降低着陆和起飞时的最低天气标准。随着机组情景识别能力的提高,必须提出高效的试飞方法来验证情景识别系统的适航符合性,在分析EVS、SVS与HUD结合使用的基础上,提出综合的优化的民用飞机机组情景识别系统试飞方法以及基于任务的符合性判据。For the excellent situation display ability of head up display, enhanced vision display and synthetic vi-sion display, the ability of pilot＇s situation recognition and perception will be obviously enhanced by using them to-gether. Simultaneously, head up display （ HUD） combined with automatic landing system can decrease the mini-mum weather standard of takeoff and landing. With enhanced ability of pilot＇s situation recognition ,a high effi-cient method is required to certificate the airworthiness of situation recognition system. Based on employing combi-nation of HUD and enhanced vision system （ EVS） , synthetic vision system （ SVS） , the paper proposes a combined optimum flight test method on crew situation recognition system for civil aircraft and acceptance criteria based on task.

关 键 词：平视显示器 视景增强系统 合成视景系统 情景识别系统 试飞 

分 类 号：V241.6[航空宇航科学与技术—飞行器设计]