面向软件定义的飞行器综合电子系统软件架构技术  

Software Architecture Technology of Software-Defined Spacecraft Integrated Electronic System

作　　者：王小辉[1] 张涛[2] 吕殿君[1] 詹景坤[1] Wang Xiaohui;Zhang Tao;Lv DianJun;Zhan Jingkun(Research and Development Center,China Academy of Launch Vehicle Technology,Beijing 100076,China;School of Software and Microelectronics,Northwestern Polytechnical University,Xi’an 710072,China)

机构地区：[1]中国运载火箭技术研究院研究发展中心,北京100076 [2]西北工业大学软件与微电子学院,西安710072

出　　处：《航天控制》2019年第4期66-71,共6页Aerospace Control

基　　金：上海航天科技创新基金(2017KC160011)

摘　　要：针对飞行器系统智能化发展对传统软硬件一体化研制方式的挑战,本文提出一种面向软件定义的开放式、可移植的飞行器软件体系架构。首先,提出一种逐层解耦的分段式飞行器软件体系架构,通过标准化各个段的接口与服务,实现飞行器的软硬件解耦、平台解耦与组件间解耦,有效支持飞行器软件功能组件的可移植与复用;其次,基于该软件体系架构,采用标准化可复用软件组件的快速集成验证方法,实现飞行器功能的软件定义。Aiming at the development of spacecraft intelligence which leads to the challenge of traditional software and hardware coupling development method,An open and portable spacecraft software architecture is proposed for software-defined technology. Firstly,a layer-by-layer decoupled segmented spacecraft software architecture is proposed. By standardizing the interfaces and services of each segment,the software and hardware decoupling,platform decoupling and component decoupling of the spacecraft are realized,effectively supporting the portability and reuse of spacecraft software functional components. Secondly,based on the software architecture,the software definition of spacecraft function is realized by the rapid integration verification method of standardized reusable software components.

关 键 词：软件自定义功能 开放式系统架构 可移植 飞行器综合电子系统架构 

分 类 号：E927[军事—军事装备学]