Patent · US Active

Method for configuring a distributed avionics control system

US9172589B2 · kind B2 · utility

1Cited by
3References
13Claims
0Family size

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Inventors

Key dates

Filing dateJul 5, 2010
Grant dateOct 27, 2015
Priority date
Expiry dateJul 10, 2031

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG06F9/546
  • WIPO fieldComputer technology
  • WIPO sectorElectrical engineering

Abstract

The present invention relates to a method for configuring synchronous table-driven operations of a distributed avionics control system comprising a plurality of processing nodes (S1-S4) interconnected in a network (2). The method comprises the steps of providing a global timing meta-data component (X4), a plurality of application meta-data components (X51-X52), and a node assignment meta-data component (X 2). The method also comprises the steps of detecting data communication paths, detecting communication requirements, generating a system schedule meta-data component, generating a system configuration data and providing the system configuration to the distributed avionics control system.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.