发明名称 Failure self-detection method for embarked avionic system of aircraft, involves detecting failure of system by implementing boundary defining sub-space where representation of data is associated to detection of failure, of space
摘要 <p>The method involves determining physical quantities represented by data, where the physical quantities comprise temporal quantity representing persistence of an event in time, and instantaneous quantity. The data are represented by points whose coordinates have values of the physical quantity, in a space. A failure of an embarked avionic system is detected by implementing a boundary defining a sub-space where representation of the data is associated to detection of failure, of the space. An independent claim is also included for a device for self-detection of failure in an embarked system from failure representing data, comprising a determination unit.</p>
申请公布号 FR2932583(A1) 申请公布日期 2009.12.18
申请号 FR20080053953 申请日期 2008.06.13
申请人 AIRBUS FRANCE 发明人 CHERIERE VINCENT;DOS SANTOS GIRIO JOAO ARAMIS
分类号 G06F11/30 主分类号 G06F11/30
代理机构 代理人
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