Development system for an aeronautical software application comprising a structured functional description language

The method involves realizing an executable software by a development segment of an aeronautical software application. Functional capacities of widgets created or integrated by computing units of the segment, are defined by associating consumed variables i.e. input plugs, to modifiable attributes of...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Thiry, Yannick, Leconte, Hervé, Arneau, David
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
Online-Zugang:	Volltext bestellen
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