机载系统采用COTS操作系统的适航符合性实现方法  

Preliminary Study on Avionics Integrator’s Airworthiness Compliance Using COTS Operating System

作　　者：金强[1] 裴宇鑫 黄帆 JIN Qiang;PEI Yu-xin;HUANG Fan(China Aeronautical Radio Electronics Research Institute,Shanghai 200241,China)

机构地区：[1]中国航空无线电电子研究所,上海200241

出　　处：《航空电子技术》2023年第3期68-74,共7页Avionics Technology

摘　　要：本文从民用机载系统集成方角度,提出了一种商用货架产品操作系统型号项目应用中的适航符合性方法:作为具体型号项目的产品组成部分,建议集成方采用商用货架产品操作系统评估、筛选以及设计迭代的方式,确保商用货架产品操作系统满足预期功能和型号审定的需要。该方法意图为民用机载系统集成方开展产品研制、为局方确定相关适航符合性提供参考和借鉴;也可作为商用货架产品操作系统供应商开发适合航电应用新产品的研发考虑。From the perspective of civil airborne product integration,a compliance method is proposed for COTS op-erating system:as part of an airborne product for a specific project type,it is suggested that the integrator adopt COTS operating system evaluation,screening and design iteration should ensure that the COTS operating system meets the needs of expected functions and type certification.This method is intended to provide reference for civil airborne prod-uct integrators to develop products,and for the bureau to determine relevant airworthiness compliance.And this method can be a guidance for COTS operating system suppliers to develop new products for aviation application.

关 键 词：民用机载系统 商用货架产品操作系统 集成方 适航符合性 

分 类 号：V221.91[航空宇航科学与技术—飞行器设计]