02-05-2023 дата публикации
Номер: CN116051068A
Принадлежит:
The invention discloses a satellite product maintainability time parameter prediction method, which comprises the following steps: determining system function levels and related fault modes, and carding to obtain a fault mode list; determining maintainability prediction parameters and maintenance time elements; constructing to obtain a maintainability prediction model; on the basis of the fault mode list, for each fault mode, predicting the value of each maintenance time element item by item according to the specific maintenance scheme of each fault mode; and according to the summarizing result of the predicted values of the maintenance time elements, combining with the maintainability prediction model, and calculating to obtain predicted values of the maintainability prediction parameters. According to the method, the relationship between the satellite maintenance time parameter and each maintenance time element, the on-orbit maintenance strategy, the fault rate, the single event upset ...
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