发明名称 METHOD AND SYSTEM FOR MANAGING A PLURALITY OF CRITICAL FUNCTIONS IN AN AIRCRAFT
摘要 A system and a method are disclosed for managing a plurality of critical functions in an aircraft, the system comprising at least one data providing unit for providing digital signals, wherein at least one digital signal is associated with a given critical function of the plurality of critical functions; at least one transmission path coupled to the at least one providing unit; a memory unit for storing an operating system and a plurality of critical applications managing the plurality of critical functions; and a processing unit operatively coupled to the memory unit and configured to receive the digital signals along the at least one transmission path, the processing unit for executing the operating system and the plurality of critical applications, wherein the execution of the plurality of critical applications is managed by the operating system to accommodate fast loops and to ensure independence of the plurality of critical applications.
申请公布号 CA2933064(A1) 申请公布日期 2015.06.25
申请号 CA20142933064 申请日期 2014.12.17
申请人 THALES CANADA INC. 发明人 GANSMANDEL, FRANCK;NACOUZI, JACQUES;ALEPINS, ETIENNE;NAZON, YVON;CADOTTE, PATRICK;CLEMENT, FREDERICK
分类号 B64D47/00;G06F19/00;H04L12/16 主分类号 B64D47/00
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