SATCOM data unit with wireless device

• US 9,503,175 B2
• Filed: 06/09/2014
• Issued: 11/22/2016
• Est. Priority Date: 02/03/2014
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Judd, Thomas D., Howe-Ryberg, Sandra J., Gandhi, Darshan
• Primary Examiner(s): Rachedine, Mohammed
• Application Number:
  US14/299,078
• Publication Number:
  US 20150222351A1
• Time in Patent Office: 897 Days
• US Class Current: 1/1
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system

Abstract

An aerospace communication system comprises a communication management unit; a first communication device configured to transmit and receive data over a first communication network; and a second communication device configured to transmit and receive data over a second communication network. The first communication device is coupled to a corresponding interface of the communication management unit. The second communication device is communicatively separated from the communication management unit by the first communication device such that the communication management unit is unaware of the second communication device. The first communication device includes routing logic configured to determine whether to send each message received from the communication management unit over the first communication network or to the second communication device for transmission over the second communication network.

Claims

1. An aerospace communication system comprising:

a communication management unit;

a first communication device configured to transmit and receive data over a first communication network;

a second communication device configured to transmit and receive data over a second communication network;

wherein the first communication device is in communication with a corresponding interface of the communication management unit;

wherein the first communication device is in communication with the second communication device;

wherein the second communication device is communicatively separated from the communication management unit by the first communication device such that the communication management unit is unaware of the second communication device;

wherein the first communication device includes routing logic configured to determine whether to send each message received from the communication management unit over the first communication network or to the second communication device for transmission over the second communication network; and

wherein the aerospace communication system is configured for use onboard an aircraft.

2. The aerospace communication system of claim 1, wherein the first communication device includes one of a satellite communications (SATCOM) unit, a High Frequency (HF) radio, or a Very High Frequency (VHF) radio;

and

wherein the second communication device includes at least one of a cellular radio and a Wi-Fi radio.

3. The aerospace communication system of claim 1, wherein the first communication device is configured to route uplink messages received at the second communication device to the communication management unit such that the uplink messages appear to the communication management unit to have been received via the first communication device.

4. The aerospace communication system of claim 1, wherein the second communication device and the first communication device are included in the same line replaceable unit (LRU).

5. The aerospace communication system of claim 1, wherein the first communication device includes an interface configured to couple the first communication device with the second communication device, the second communication device being physically separate from the first communication device.

6. The aerospace communication system of claim 1, wherein the routing logic in the first communication device is configured to determine whether to send each message received from the communication management unit over the first communication network or to the second communication device based on at least one of a respective cost associated with each of the first and second communications networks, availability of the respective first and second communication networks, user preference, security level, quality of service, and a respective domain associated with each message received from the communication management unit.

7. The aerospace communication system of claim 1, wherein the first communication device includes a memory configured to store each respective message for which the communication network selected by the routing logic in the first communication device is unavailable, wherein the first communication device is configured to store each respective message until the selected communication network corresponding to each respective stored message becomes available.

8. An aerospace communication unit comprising:

an interface configured to communicatively couple the aerospace communication unit to a communication management unit;

a first communication radio configured to transmit data over a first communication network;

routing logic configured to determine whether to route messages received from the communication management unit to the first communication radio or to a second communication radio configured to transmit data over a second communication network;

wherein the routing logic is configured to determine whether to route messages to the first communication radio or the second communication radio independent of routing decisions performed by the communication management unit such that the second communication radio is hidden from the communication management unit; and

wherein the aerospace communication system is configured for use onboard an aircraft.

9. The aerospace communication unit of claim 8, further comprising a second interface configured to communicatively couple the aerospace communication unit to the second communication radio.

10. The aerospace communication unit of claim 8, wherein the aerospace communication unit includes the second communication radio.

11. The aerospace communication unit of claim 8, wherein the first communication radio comprises one of a high frequency (HF) radio, a very high frequency (VHF) radio, and a satellite communication (SATCOM) radio;

and

wherein the second communication radio comprises at least one of a cellular radio and a Wi-Fi radio.

12. The aerospace communication unit of claim 8, wherein the first communication radio is configured to route uplink messages received at the second communication radio to the communication management unit such that the uplink messages appear to the communication management unit to have been received via the first communication radio.

13. The aerospace communication unit of claim 8, wherein the routing logic is configured to determine whether to route the messages received from the communication management unit to the first communication radio or to the second communication radio based on at least one of a respective cost associated with each of the first and second communications networks, availability of the respective first and second communication networks, user preference, security level, quality of service, and a respective domain associated with each message received from the communication management unit.

14. The aerospace communication unit of claim 8, further comprising:

a memory configured to store each message for which the communication network selected by the routing logic is unavailable until the selected communication network corresponding to each respective stored message becomes available.

15. A method of communicating a message from an aircraft, the method comprising:

receiving a message at a first unit onboard the aircraft, the first unit configured to route messages for transmission to a ground station, the message from a device onboard the aircraft;

selecting, at the first unit, one of a plurality of communication devices onboard the aircraft for transmission of the message to the ground station, the first unit including a corresponding interface for each communication device in the plurality of communication devices;

wherein the plurality of communication devices includes a first communication device associated with at least one additional communication device that does not have a corresponding interface in the first unit such that the first unit is unaware of the at least one additional communication device;

sending the message from the first unit to the selected communication device over the respective interface of the first unit corresponding to the selected communication device; and

when the message is sent over the respective interface corresponding to the first communication device, routing the message after leaving the first unit to one of the at least one additional communication device or to the first communication device for transmission to the ground station.

16. The method of claim 15, wherein the first communication device comprises one of a satellite communications (SATCOM) unit, a High Frequency (HF) radio, or a Very High Frequency (VHF) radio;

and

wherein the at least one additional communication device includes at least one of a cellular radio and a Wi-Fi radio.

17. The method of claim 15, further comprising routing, in the first communication device, uplink messages received at the at least one additional communication device to the first unit such that the uplink messages appear to the first unit to have been received at the first communication device.

18. The method of claim 15, wherein routing the message after leaving the first unit to one of the at least one additional communication device or to the first communication device for transmission to the ground station comprises:

receiving the message at a router communicatively coupled between the first unit and the first communication device; and

selecting one of the at least one additional communication device or the first communication device at the router.

19. The method of claim 15, wherein routing the message after leaving the first unit to one of the at least one additional communication device or to the first communication device for transmission to the ground station comprises:

receiving the message at the first communication device; and

selecting one of the at least one additional communication device or the first communication device at the first communication device.

20. The method of claim 19, further comprising sending the message over an interface of the first communication device communicatively coupled to the at least one additional communication device when the at least one additional communication device is selected.

21. An aerospace communication system comprising:

a communication management unit;

a first communication device configured to transmit and receive data over a first communication network;

a second communication device configured to transmit and receive data over a second communication network;

a routing device in communication with both the first communication device and the second communication device;

wherein the routing device is also in communication with a corresponding interface of the communication management unit;

wherein the routing device separates the second communication device from the communication management unit such that the communication management unit is unaware of the second communication device;

wherein the routing device includes routing logic configured to determine whether to send each message received from the communication management unit to the first communication device for transmission over the first communication network or to the second communication device for transmission over the second communication network; and

wherein the aerospace communication system is configured for use onboard an aircraft.