首页> 外国专利> 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

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

机译:用于飞机的机载航空电子系统的故障自检测方法,涉及通过实现边界定义子空间来检测系统的故障,其中数据表示与空间的故障检测相关联

摘要

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.
机译:该方法涉及确定由数据表示的物理量,其中物理量包括表示事件在时间上的持续性的时间量和瞬时量。数据由点表示,这些点的坐标在空间中具有物理量的值。通过实现定义子空间的边界,可以检测出飞机上的航空电子系统的故障,其中数据的表示与该空间的故障的检测相关联。还包括一种独立权利要求,用于从故障代表数据中自我检测登船系统中的故障的设备,该设备包括确定单元。

著录项

  • 公开/公告号FR2932583A1

    专利类型

  • 公开/公告日2009-12-18

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号FR20080053953

  • 申请日2008-06-13

  • 分类号G06F11/30;

  • 国家 FR

  • 入库时间 2022-08-21 18:26:48

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