公开(公告)号：US20170011636A1

公开(公告)日：2017-01-12

申请号：US15202513

申请日：2016-07-05

Applicant: THALES

Inventor： François NEFFLIER ,  Hervé AULFINGER ,  Patrick PIERRE

IPC: G08G5/00 ,  H04L29/08

CPC classification number: G08G5/0034 ,  G06F8/20 ,  G08G5/0017 ,  H04L67/12

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.

Abstract translation: 用于集成受限航空器路线优化应用的方法在包括用于管理该应用的DAL +核心计算机和DAL-外围计算机的航空电子系统中实现。 集成方法根据几个参数确定了车载航空电子系统中应用程序的基本函数OPT_RTE_FU（i）的最优功能和物理分布，这些可能分布使全球成本标准CG最小化，这取决于几个参数，包括至少 将基本功能的额外开发成本集成在DAL +数字核心计算机内，并进行应用的集成。