AIRCRAFT INTEGRATED MULTI SYSTEM ELECTRONIC ARCHITECTURE

AIRCRAFT INTEGRATED MULTI SYSTEM ELECTRONIC ARCHITECTURE

A flexible distributed multi-system architecture for aircraft control integrates electronic computers comprising plural types of high integrity, dissimilar, generic and reconfigurable controllers (GECs) that can assume different purposes. GECs are configured as actuator controllers (able to control...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: GALVÃO, Marcelo, CAMPOS, Marcos Vinicius, MARENGO, Luiz Carlos
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
CALCULATING
COMPUTING
COSMONAUTICS
COUNTING
ELECTRIC DIGITAL DATA PROCESSING
HELICOPTERS
PERFORMING OPERATIONS
PHYSICS
TRANSPORTING
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Beschreibung
Zusammenfassung:A flexible distributed multi-system architecture for aircraft control integrates electronic computers comprising plural types of high integrity, dissimilar, generic and reconfigurable controllers (GECs) that can assume different purposes. GECs are configured as actuator controllers (able to control up to three channels including hydraulic or electro-mechanical actuators) or as Control Law Computers (able to calculate more sophisticated and processor demanding control laws). The multi-system architecture is built around a backbone of high performance, high integrity digital protocols and three hubs with dual connection to two different GECs.