Testability simulation method based on aviation airborne system function performance model

The invention relates to a testability simulation method based on a functional performance model of an aviation airborne system, which comprises the following steps: S1, acquiring information of the functional performance model of the aviation airborne system, and carrying out testability simulation...

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Bibliographische Detailangaben
Hauptverfasser: YE ZHAOBIN, CHEN CHEN, SONG BO, JIANG JUEYI, PENG WEIJIE
Format: Patent
Sprache:chi ; eng
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