Aircraft radio system
View Patent ↗An aircraft radio system comprising a plurality of radios interconnected by a digital communications network, each radio having a transceiver and a dedicated processor platform, the aircraft radio system being configured to cause the dedicated processor platforms to constitute a virtual processing environment for the aircraft radio system. There is also an aircraft radio system comprising a plurality of discrete radios interconnected by a digital communications network, each radio having a transceiver, a dedicated processor platform and a server configured to support communications over the network using PPPoE, Point to Point Protocol over Ethernet, to provide a common digital interface between an aircraft domain and the radios for plural types of communication.
1. An aircraft radio system comprising:
a plurality of radios, each radio having a transceiver and a dedicated processor platform to carry out waveform processing for the transceiver;
the dedicated processor platforms being interconnected to one another through a digital communications network such that the dedicated processor platforms constitute a virtual processing environment for the aircraft radio system,
wherein, within the virtual processing environment, processing of an individual waveform received by a first one of the transceivers is distributed across at least two of the dedicated processor platforms, such that the processing of the individual waveform is carried out in part by the processor platform dedicated to the first one of the transceivers and in part by one or more of the processor platforms that are dedicated to other ones of the transceivers.
2. The system according to claim 1 , wherein at least one of the dedicated processor platforms is dedicated to two or more of the transceivers.
3. The system according to claim 1 , wherein two or more of the dedicated processor platforms are grouped in a module separate from the transceivers.
4. The system according to claim 1 , wherein the network is a deterministic network.
5. The system according to claim 1 , wherein the network is an Ethernet network.
6. The system according to claim 1 , wherein the virtual processing environment complies with at least one of Common Object Request Broker Architecture (CORBA) or Real-Time CORBA.
7. The system according to claim 1 , wherein at least one of the radios employs Software Defined Radio techniques.
8. The system according to claim 1 , wherein the system is configured to cause two or more of the dedicated processor platforms to constitute a virtual processing environment for seamless networking over multiple possible radio channels.
9. The system according to claim 1 , wherein the system is configured to cause two or more of the dedicated processor platforms to constitute a virtual processing environment for radio management.
10. The system according to claim 1 , wherein the dedicated processor platforms have a common architecture, including at least one of: a common hardware architecture; common interfaces; a common development environment; or a common software execution environment.
11. The system according to claim 1 , wherein each radio comprises a transceiver module interfacing with the dedicated processor platform via an interface common to the radios.
12. The system according to claim 1 , further comprising:
a server configured to support communications over the network using Point to Point Protocol over Ethernet (PPPoE) to provide a common digital interface between an aircraft domain and the radios for plural types of communication.
13. The system according to claim 1 , further comprising at least one controller interfacing with the network, each controller being configured to determine its own overall connectivity and to broadcast this over the network to allow client systems to select a controller for use, based on the ranking of connectivities.
14. The system according to claim 13 , wherein each controller is configured to determine its connectivity based on the type of radio service it is able to offer and a priority level established and stored when the aircraft radio system is commissioned or configured.
15. The system according to claim 1 , further comprising a plurality of antenna systems each connected to a respective radio by a Radio Frequency (RF) cable link.
16. The system according to claim 1 , further comprising:
cabin and cockpit human-machine interfaces and avionics interfaces, interconnected with the plurality of radios through the digital communications network.
17. The system according to claim 4 , wherein the deterministic network is an Avionics Full Duplex Ethernet (AFDX) network.