Patent · US Active

Method and system for monitoring a graphical interface in an aircraft cockpit

US9195375B2 · kind B2 · utility

3Cited by
1References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 3, 2012
Grant dateNov 24, 2015
Priority date
Expiry dateOct 21, 2033

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG06F11/3089
  • WIPO fieldComputer technology
  • WIPO sectorElectrical engineering

Abstract

The invention relates in particular to a method and a system for monitoring a graphical interface in a computer system of an aircraft cockpit. The method comprises, in addition to the display of a graphical interface of a client application based on a tree structure of graphical interaction objects composing said graphical interface, the following steps: obtaining a plurality of graphical interaction objects having a tree-structure organization; creating and adding, to said obtained tree structure, at least one new graphical interaction object defining a critical graphical display zone; modifying the tree-structure dependency of at least one critical graphical interaction object, of the obtained tree structure to make it dependent from the new graphical interaction object defining the critical zone; and performing critical monitoring only of the critical graphical objects attached to the critical zone.

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