公开(公告)号：US10147327B2

公开(公告)日：2018-12-04

申请号：US15202513

申请日：2016-07-05

Applicant: THALES

Inventor： François Nefflier ,  Hervé Aulfinger ,  Patrick Pierre

IPC: G08G5/00 ,  H04L29/08 ,  G06F8/20

Abstract: A method for integrating a constrained aircraft route(s) optimization application is implemented in an avionics onboard system comprising a DAL+ core computer and a DAL− peripheral computer for managing the application. The method of integration determines an optimal functional and physical distribution of the elementary functions OPT_RTE_FU(i) of the application within the onboard avionics system over the set of possible distributions which minimizes a global cost criterion CG, dependent on several parameters, including at least the additional development cost of the elementary functions integrated within the DAL+ digital core computer, and carries out the integration of the application.

公开(公告)号：US10699582B2

公开(公告)日：2020-06-30

申请号：US16009017

申请日：2018-06-14

Applicant: THALES

Inventor： Benoît Dacre-Wright ,  Olivier Pineau ,  François Nefflier

IPC: G08G5/00 ,  G02B27/01 ,  G01C21/20 ,  G01C23/00

Abstract: Various methods for regulating and/or for integrating avionic systems with non-avionic systems are described. An avionic system is generally associated with a physical fault rate that is lower and a logic verification that is higher than those of a non-avionic system. Developments describe notably the use: of remote computing resources; of comparison, test, verification and authorization steps before injection of data of non-avionic origin into the avionics; of human-machine interaction methods; of various parameters (weather, air traffic, etc.) for the purpose of combinatorial optimization; and of electronic flight bags EFB and of flight management systems FMS.