Aircraft control system with merged links
AssigneeAirbus Operations GmbH
InventorsMarc FERVEL, Antoine MAUSSION, Arnaud LECANU, Sylvain SAUVANT
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AssigneeAirbus Operations GmbH
InventorsMarc FERVEL, Antoine MAUSSION, Arnaud LECANU, Sylvain SAUVANT
Estimating the term…
The invention relates to an aircraft control system, situated in the avionics bay, including a computer, a remote equipment, such as an actuator of control surfaces, and an AFDX network. The computer includes a first module and a second module, respectively connected to a corresponding first module and a second module of the equipment, by a first and a second virtual link sharing a common path through the network, the first and second virtual links being segregated by a separate encoding at the applicative level. A replication and/or frame switching device is connected, on the one hand, to the common port and, on the other hand, to the ports of the first and second modules of the equipment.
An aircraft control system comprising a computer and a remote equipment, the computer comprising a first and a second module, the first module of the computer being connected to a first module of said equipment through an AFDX network by a first virtual link, and the second module of the computer being connected to a second module of said equipment by a second virtual link through this same network, characterised in that:
Dependencies are inferred from the claim text.