军用飞机飞行管理系统适航性应用研究  

Application Research on Airworthiness of Flight Management System for Military Aircraft

作　　者：祖肇梓 雷宏杰[1] 屈重君[1] Zu Zhaozi;Lei Hongjie;Qu Zhongjun(AVIC Xi’an Flight Automatic Control Research Institute,Xi’an 710065,China)

机构地区：[1]航空工业西安飞行自动控制研究所,西安710065

出　　处：《航空兵器》2020年第6期25-29,共5页Aero Weaponry

摘　　要：在军用飞机飞行管理系统中开展适航性工作,是飞行管理系统研制过程中的难点之一。本文通过研究国外军用飞机适航性和飞行管理系统在军用飞机上的应用现状,对比分析我国军用飞机开展适航性的现状和难点,确定我国军用飞机飞行管理系统的适航性在设计研制过程中需遵循的规范和标准。此外,对军用飞机型号研制中开展飞行管理系统适航性的安全性做了分析,并对飞行管理系统适航性实现的设计要求和管理要求进行分析,探索了在我国现行的军用飞机机载产品的研制体系下,如何开展军用飞机飞行管理系统适航性工作。The airworthiness study for military aircraft flight management system(FMS)is one of the crucial difficulties for the FMS research and development.This article analyzes the current application situations and difficulties of the airworthiness work for the military FMS in China in contrast with that in other countries,and researches the airworthiness standards and specifications that are necessary to comply with in the design and development process of the domestic military FMS.Meanwhile,this article analyzes safety assurance,design requirements and management specifications of the airworthiness work for the research and development of the military FMS.Accordingly,this article explores the approach and methodology of the airworthiness work for the military FMS based on the current research and development system of the domestic military onboard products.

关 键 词：军用飞机 适航性 飞行管理系统 安全性 适航体系 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计] V249.32