摘要
针对航天器控制系统软件特性及交会对接任务特点,利用软件可靠性理论,研究提高软件可靠性的方法,提出了面向交会对接任务软件的可靠性设计,增强了航天器控制系统的可靠性。
In view of the characteristics of spacecraft control system software and spacecraft rendezvous and docking （ RVD ） , several methods for enhancing software reliability are proposed by using the software reliability theory in this paper. The reliability design of the RVD mission software is proposed, which enhances the spacecraft control system reliability.
出处
《航天控制》
CSCD
北大核心
2013年第1期38-43,共6页
Aerospace Control
关键词
交会对接
控制系统
应用软件
软件可靠性
Rendezvous and docking（RVD）
Control system
Application software
Software reliability
