Satellite emergency voice/data downlink

• US 6,385,513 B1
• Filed: 11/22/1999
• Issued: 05/07/2002
• Est. Priority Date: 12/08/1998
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Honeywell International Inc.
• Inventors: Murray, William W., Cessna, John
• Primary Examiner(s): Beaulieu, Yonel
• Application Number:
  US09/444,540
• Time in Patent Office: 897 Days
• Field of Search: 701/14, 701/15, 701/16, 701/17, 701/18, 701/200, 342/33, 342/34, 342/35, 342/36, 342/37, 342/29, 340/945, 340/947, 340/951, 340/971, 340/973, 244/76.R
• US Class Current: 701/14
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0026 located on the ground
• CPC Class Codes: G08G 5/0056 in an emergency situation, e.g. hijacking
• CPC Class Codes: H04B 7/18508 with satellite system used as relay, i.e. aeronautical mobile satellite service

Abstract

A satellite emergency voice/data downlink method and apparatus that sends cockpit audio and flight data to a satellite communications system upon detection of a serious event or a pilot generated signal.

Claims

1. An airborne distress link apparatus for an airplane having on board one or more communications systems, said apparatus comprising:

means for establishing an event marker;

means for detecting an emergency situation; and

a processor having one or more inputs receiving inputs representative of one or more flight conditions and one or more outputs coupled to one or more on-board communications systems, said processor having an algorithm resident thereon for initiating a downlink of one or more flight data using one or more of said communications systems in response to the activation of said means for establishing an event marker or said means for detecting an emergency situation.

2. The airborne distress link apparatus recited in claim 1, wherein said processor is a component of one of said one or more communications systems.

3. The airborne distress link apparatus recited in claim 1, wherein said processor is a component of one or more avionics modules coupled to one of said one or more communications systems.

4. The airborne distress link apparatus recited in claim 1, wherein said processor is configured as a stand-alone avionics module.

5. A method for transmitting flight data in an aircraft communications device to a ground based data storage center via a satellite communications system and using one or more on-board communications systems, said method comprising then steps of:

monitoring one or more flight parameters;

determining an abnormal condition in response to said monitoring step; and

automatically initiating a downlink of said flight data in response to said step of determining said abnormal condition.

6. The method recited in claim 5, said method further comprising

arranging said flight data into data packets for transmission by said one or more on-board communications systems and

determining the operability of each of said on board communication systems.

7. The method recited in claim 5, further comprising the step of activating an event marker and wherein said initiating a downlink is further responsive to an activation of said event marker.

8. The method recited in claim 5, wherein said determining an abnormal condition further comprises determining one or more of a plurality of predetermined emergency conditions.

9. The method recited in claim 5, wherein said initiating a downlink of flight data further comprises initiating a downlink of cockpit audio data.

10. The method recited in claim 5, wherein said one or more on-board communications systems comprise a satellite telecommunications unit, a telephone-based satellite communication system, and a radio data link.

11. The method recited in claim 6, wherein said arranging said flight data into data packets for transmission further comprises arranging said flight data into said data packets as a function of said determined operability of said on-board communications systems.

12. The method recited in claim 11, wherein said arranging said flight data into said data packets further comprises assigning different ones of said data packets to different operable ones of said on-board communications systems.

13. A method in an aircraft communications device for determining a serious event and transmitting flight data in response to the serious event, the method comprising:

receiving one or more signals triggering a distress mode;

collecting flight data into data packets in response to said triggering step; and

automatically initiating a downlink of selected ones of said flight data via a satellite communication system and utilizing one or more on-board communications systems.

14. The method recited in claim 13, wherein said one or more signals triggering a distress mode includes one or more of an event marker signal, a signal representative of one of one or more predetermined emergency situations, and a signal representative of another serious event.

15. The method recited in claim 14, wherein said signal representative of one of one or more predetermined emergency situations further comprises a predetermined one or more of out-of-limit announcements generated by an on-board fault computer.

16. The method recited in claim 14, wherein said signal representative of one of one or more predetermined emergency situations further comprises a signal representative of an out-of-limit condition generated by predetermined ones of a plurality of on-board flight sensors.