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故障管理功能缺乏系统性的设计方法,是航天运载器健康管理系统设计面临的普遍问题之一。提出一种面向故障影响控制的航天运载器故障管理功能设计方法,并结合某型运载器故障管理功能设计对该方法的工程应用进行初步探讨。
The lack of a systematic design approach to fault management functions is one of the common problems facing the design of a space vehicle health management system. A design method of fault management for aerospace vehicle based on fault influence control is proposed. The engineering application of this method is discussed based on the fault management of a certain type of vehicle.