PROCEDE D'INTEGRATION D'UN NOUVEAU SERVICE DE NAVIGATION DANS UN SYSTEME AVIONIQUE EMBARQUE A ARCHITECTURE OUVERTE DE TYPE CLIENT-SERVEUR, EN PARTICULIER D'UN SERVICE DE MANOEUVRE FIM

A method for integrating a new navigation service 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...

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Bibliographische Detailangaben
Hauptverfasser:	DEWEERDT, LAURENT, COULMEAU, FRANCOIS
Format:	Patent
Sprache:	fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CALCULATING COMPUTING COSMONAUTICS COUNTING ELECTRIC DIGITAL DATA PROCESSING EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PARACHUTES PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	A method for integrating a new navigation service 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 FU(i) of the new service 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 digital DAL+ core computer, and carries out the integration of the new service.