首页 | 本学科首页   官方微博 | 高级检索  
     检索      

航天器控制软件可靠性工程方法研究
引用本文:奚坤,王振华,蔡雨辰,陈朝晖.航天器控制软件可靠性工程方法研究[J].空间控制技术与应用,2016,42(4):48-52.
作者姓名:奚坤  王振华  蔡雨辰  陈朝晖
作者单位:北京控制工程研究所;北京控制工程研究所;北京控制工程研究所;北京控制工程研究所
基金项目:国家高技术研究发展计划(863)资助项目(2015AA7046306)
摘    要:当前航天器控制软件的复杂度越来越高,软件的规模十分庞大,对软件可靠性安全性要求极高,因此对航天器控制软件的可靠性设计和度量具有重要意义.介绍和分析适用于航天器控制软件的可靠性设计方法,并结合某型号给出实际的软件设计以及可靠性度量的具体实例.

关 键 词:航天器控制软件  导航制导控制  软件可靠性设计  可靠性度量

Reliability Engineering Method on Spacecraft Control Software
XI Kun,WANG Zhenhu,CAI Yuchen and CHEN Zhaohui.Reliability Engineering Method on Spacecraft Control Software[J].Aerospace Contrd and Application,2016,42(4):48-52.
Authors:XI Kun  WANG Zhenhu  CAI Yuchen and CHEN Zhaohui
Institution:Beijing Institute of Control Engineering, Beijing 100190,;Beijing Institute of Control Engineering, Beijing 100190,;Beijing Institute of Control Engineering, Beijing 100190,;Beijing Institute of Control Engineering, Beijing 100190,
Abstract:The spacecraft control software is becoming more complex and huge now, which requires higher software reliability and security and leads to higher demands on both reliability design and measure of spacecraft control software. In this paper, a reliability design method, which is suitable for space application, is given and analyzed. Based on a certain aerospace combined with concrete examples of the reliability measure, the software design is proposed.
Keywords:spacecraft control software  guidance navigation control  software reliability design  reliability measure
本文献已被 CNKI 等数据库收录!
点击此处可从《空间控制技术与应用》浏览原始摘要信息
点击此处可从《空间控制技术与应用》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号