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.
PROCEDE D'INTEGRATION D'UNE APPLICATION D'OPTIMISATION DE ROUTE (S) SOUS CONTRAINTES DANS UN SYSTEME EMBARQUE AVIONIQUE A ARCHITECTURE OUVERTE DE TYPE CLIENT SERVEUR
11.05.2018
Patent
Elektronische Ressource
Französisch
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