摘要
为提高发动机试车控制软件的可靠性,通过需求分析、概要设计、详细设计、软件测试等步骤实现了软件开发工程化。结合试验控制软件研制和使用特点,对软件质量管理的具体步骤,即从设计评审、测试、验证、文档及技术状态管理等方面对软件开发过程进行监督与管理,实现了软件开发的质量控制,达到了软件设计的透明性、继承性及高可靠性。
To improve reliability of the control software for rocket engine test, an engineering method is introduced into the developing process of the software through requirement analysis, brief design, detail design and software testing. Also quality management approaches are carried out considering the features of development and application of the software, which are supervising and managing the developing process from the aspects of review, test, validation, documenting and technical status control. All the measures reach the goal of high reliability software development.
出处
《火箭推进》
CAS
2008年第4期60-64,共5页
Journal of Rocket Propulsion
关键词
火箭发动机
试验
控制软件
可靠性
质量管理
rocket engine
experiment
control software
reliability
quality control
