Integrated avionics systems and methods

Patent metadata

Field	Value
Publication number	US-9706508-B2
Application number	US-201313857890-A
Country	US
Kind code	B2
Filing date	Apr 5, 2013
Priority date	Apr 5, 2013
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

Systems and methods are described for synchronizing data in a mobile platform. In one embodiment, a method for synchronizing data in a mobile platform is provided. The method includes: receiving a first synchronization signal at a first remote interface unit from a signal generator; receiving a second synchronization signal at a second remote interface unit from the signal generator; and executing a synchronization state machine of the first and second remote interface units based on the first and second synchronization signals to synchronize outputs of the first and second remote interface units.

First claim

What is claimed is:

1. A method for synchronizing data in a mobile platform including a flight computer without using the flight computer for the data synchronization, comprising:
receiving a first synchronization signal at a first remote interface unit apart from the flight computer from a signal generator at a first time;
receiving a second synchronization signal at a second remote interface unit apart from the flight computer that is different than the first remote interface unit, the second synchronization signal being received from the signal generator at a time that is identical to the first time;
presenting data, to a flight computer for communication, which is synchronized based on a first and second synchronizing signal wherein the flight computer is configured for providing the data communication but not for the data synchronization;
and
executing a synchronization state machine of the first and second remote interface units based on the first and second synchronization signals, and without use of the flight computer, to synchronize at an identical time an output of the first remote interface unit and an output of the second remote interface unit.

2. The method of claim 1 , further comprising generating the first synchronization signal using a first switch; and generating the second synchronization signal using a second switch.

3. The method of claim 2 , wherein the first switch is a ethernet switch, and wherein the second switch is a ethernet switch.

4. The method of claim 1 , further comprising generating the first synchronization signal using a first clock; and generating the second synchronization signal using a second clock.

5. The method of claim 4 , wherein the first and second clocks are de-bounced discrete timers.

6. The method of claim 1 , further comprising receiving inputs at a same time to the first and second remote interface units based on the first and second synchronization signals.

7. The method of claim 1 , further comprising synchronizing bus actions of the first and second remote interface units based on the based on the first and second synchronization signals.

8. A system for synchronizing data in a mobile platform including a flight computer without using the flight computer for the data synchronization, comprising:
a synchronization signal generator that generates a first synchronization signal and a second synchronization signal;
a first remote interface unit apart from the flight computer that receives the first synchronization signal at a first time and that executes at least one synchronization state machine based on the first synchronization signal; and
a second remote interface unit apart from the flight computer that is different than the first remote interface unit, that receives the second synchronization signal at a time that is identical to the first time and that executes at least one synchronization state machine based on the second synchronization signal to synchronize at an identical time an output of the second remote interface unit with an output of the first remote interface unit; and
presenting data, to the flight computer for communication, which is synchronized based on the first and second synchronizing signal wherein the flight computer is configured for providing the data communication but not for the data synchronization.

9. The system of claim 8 , wherein the synchronization signal generator includes a first switch that generates the first system synchronization signal, a second switch that generates the second system synchronization signal.

10. The system of claim 9 , wherein the first switch is a ethernet switch, and wherein the second switch is a ethernet switch.

11. The system of claim 8 , wherein the synchronization signal generator includes a first clock that generates the first system synchronization signal, and a second clock that generates the second system synchronization signal.

12. The system of claim 8 , wherein the first and second clocks are de-bounced discrete timers.

13. The system of claim 8 , wherein the first remote interface unit receives inputs at a same time as the second remote interface unit based on the first and second synchronization signals.

14. The system of claim 8 , wherein the first remote interface unit synchronizes bus actions of the first and second remote interface units based on the first and second synchronization signals.

15. An avionic system of a mobile platform including a flight computer without using the flight computer for synchronizing redundant data, comprising:
a plurality of sensor systems that transmit the redundant data;
a plurality of actuator systems that receive the redundant data;
a synchronization signal generator that generates at least two synchronization signals; and
at least two different remote interface unit controllers that are coupled by redundant data paths between the plurality of sensor systems and the plurality of actuator systems, and that synchronize at an identical time the redundant data from the plurality of sensor systems and the redundant data to the actuator systems based on at least two synchronization signals that are received at identical times; and
a flight computer that receives the redundant data which is synchronized based on the first and second synchronizing signal wherein the flight computer is configured for providing data communication based on the redundant data having been synchronized at the identical time.

16. The avionics system of claim 15 , wherein the synchronization signal generator includes at least two ethernet switches.

17. The avionics system of claim 15 , wherein the synchronization signal generator includes at least two de-bounced discrete timers.

Assignees

• Honeywell Int Inc

Inventors

• Fletcher Mitch
• Kreider Thom
• Rupp Walter Edward

Classifications

• H04W56/001 Primary

  Synchronization between nodes · CPC title

• H04B7/18506

  Communications with or from aircraft, i.e. aeronautical mobile service · CPC title