中国科技核心期刊

中文核心期刊

CSCD来源期刊

空间控制技术与应用 ›› 2016, Vol. 42 ›› Issue (4): 48-.doi: 10.3969/j.issn.1674-1579.2016.04.009

• 技术交流 • 上一篇    下一篇

航天器控制软件可靠性工程方法研究

  

  • 出版日期:2016-08-24 发布日期:2016-09-08

Reliability Engineering Method on Spacecraft Control Software

  • Online:2016-08-24 Published:2016-09-08

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

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.

Key words: spacecraft control software, guidancenavigation control, software reliability design, reliability measure

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