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介绍一种用于控制极低温、高真空模拟太空环境试验的组态软件[1] 开发方法 ,描述了ONSPEC32平台的实时数据库[1] ,详细说明了系统软件的层次结构化设计 ,为提高可靠性而采取的控制模块扇入 (fan in)扇出 (fan out)的设计及增强模块独立性设计等。
This paper introduces a development method of configuration software [1] for controlling the test of space environment at very low temperature and high vacuum. It describes the ONSPEC32 platform’s real-time database [1], and details the hierarchical structure design of the system software. In order to improve the reliability The control module fan-in fan-out design and enhance module independence design.