System and method for operating software in a flight simulator environment

• US 7,188,059 B2
• Filed: 02/19/2002
• Issued: 03/06/2007
• Est. Priority Date: 02/17/2001
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: White, Daryl A., Oss, deceased, Olsen, legal representative, Schense, Steve J., Swart, Earl
• Primary Examiner(s): Phan; Thai
• Application Number:
  US10/080,196
• Publication Number:
  US 20030023740A1
• Time in Patent Office: 1,841 Days
• Field of Search: 703/13,25 701/202 709/224,232 702/121-122
• US Class Current: 703/13
• CPC Class Codes: H04L 67/131 Protocols for games, networked simulations or virtual reality
• CPC Class Codes: H04L 9/40 Network security protocols

Abstract

The present invention is directed to a system and method for establishing communication between a flight simulator and a secondary control system, such as a Flight Management System (“FMS”). Information can be transmitted between the flight simulator and the secondary control system via a socket in a TCP/IP connection between the two systems. In the event that the secondary control system does not natively communicate in TCP/IP format, the information must be translated to and from the TCP/IP format. In this manner, an actual deliverable version of the secondary control system, possibly operating on can be used.

Claims

1. A method of exchanging information between a first computer system to a second computer system in a flight simulator environment, the method comprising:

transmitting in a network communication format an initial connection string from said first computer system to said second computer system, the initial connection string identifying said first computer system;

transmitting in a network communication format a first orientation message from said second computer system to said first computer system;

sending in a network communication format a second orientation message from said first computer system to said second computer system; and

sending in a network communication format various informational messages from said first computer to said second computer.

2. The method of claim 1 wherein said second computer is a flight simulator system.

3. The method of claim 1 wherein said first computer is a Flight Management System computer.

4. The method of claim 1 wherein

said first computer communicates in an ARINC 429 format;

said second computer communicates in a TCP/IP format; and

said method further comprises;

translating information from ARINC 429 format to TCP/IP format prior to sending information from said first computer to said second computer; and

translating information from TCP/IP format to ARINC 429 format subsequent to sending information from said second computer to said first computer.

5. The method of claim 1 wherein,

said informational messages comprises data indicating an end of frame.

6. The method of claim 1 wherein said informational messages comprises data indicating a version number.

7. The method of claim 1 wherein said informational message comprises an indication of the length of the messages.

8. The method of claim 1 wherein said information messages comprise data formatted in frames.

9. The method of claim 8 wherein said frames contain a representation of data at a specific moment in time.

10. The method of claim 9 wherein said frames are periodic.

11. The method of claim 10 wherein the period of said frames ranges from approximately 25 to 30 milliseconds.

12. A flight simulator system comprising:

a first computer;

a second computer coupled to said first computer, wherein

said first computer is configured to communicate in a first data format and further configured to transmit an initial connection string identifying said first computer to said second computer,

said second computer is configured to communicate in a second data format and is configured to transmit a first orientation message to said first computer upon receiving said initial connection string, said first computer further configured to transmit a second orientation message to said second computer upon receiving said first orientation message; and

data is transmitted between said first computer and said second computer in a network communication format.

13. The flight simulator system of claim 12 wherein

said first computer is configured to translate data between said first data format and said second data format.

14. The flight simulator system of claim 13 wherein

said second computer is configured to translate data between said first data format and said second data format.

15. The flight simulator system of claim 12 wherein said second computer is configured to process flight management system commands.

16. The flight simulator system of claim 15 wherein said second computer is configured to operate software identical to software used in aircraft systems.

17. The flight simulator system of claim 15 further comprising:

an input simulator coupled to said second computer, wherein said input simulator is configured to accept inputs from a user and transmit said inputs to said second computer.