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本文主要介绍某空间微计算机可靠性设计的基本程序,即飞行器系统对微计算机可靠性的要求及故障判据;确定可靠性模型及可靠性分配和预估;保证整机固有可靠性的设计以及提出了元件的筛选方法和整机可靠性试验规范等。
This article mainly introduces the basic procedure of the reliability design of a micro-computer in space, that is, the reliability requirements and fault criteria of the micro-computer in the aircraft system; the reliability model and the reliability allocation and prediction; the design of the inherent reliability of the whole machine; Proposed component screening method and machine reliability test specification.