民用飞机卫星通信系统的设计和适航验证考虑  

Design Consideration and Airworthiness Validation of the Satellite Communication System for Civil Aircraft

作　　者：黄跃智 张利辉[1] 

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《民用飞机设计与研究》2016年第3期69-72,共4页Civil Aircraft Design & Research

摘　　要：随着我国航空事业的快速发展,关于机载卫星通信的业务需求越来越强烈。卫星通信覆盖面积大、通信容量大、通信距离远、机动灵活、传输线路稳定可靠,是克服现有甚高频、高频通信系统局限性的最佳选择。首先对卫星通信系统进行了概述,在此基础上全面论述了卫星通信系统设计过程的考虑事项、并提出适航符合性验证的方法建议,为民用飞机卫星通信系统的适航批准提供支持。With the rapid development of the civil aviation, the airborne satellite communication is used more widely. According to the larger coverage area, it is the best choice to supplement the very high frequency and high frequency communication system. This paper firstly describes the satellite communication, and provides a general design consideration and means of compliance, in order to support the airworthiness approval of the satellite equipment.

关 键 词：卫星通信 设计考虑 适航验证 

分 类 号：V243.1[航空宇航科学与技术—飞行器设计]