Systems and methods for asynchronous telemetry bandwidth simulator

Patent metadata

Field	Value
Publication number	US-2025138895-A1
Application number	US-202418636593-A
Country	US
Kind code	A1
Filing date	Apr 16, 2024
Priority date	Oct 30, 2023
Publication date	May 1, 2025
Grant date	—

Abstract

A method, computer program product, and computer system for identifying, by a computing device, a plurality of information associated with a flight simulation. A plurality of frame arrivals can be constructed based upon, at least in part, the plurality of information associated with the flight simulation. The plurality of frame arrivals can be packetized into a plurality of data packets. The plurality of data packets can be multiplexed to generate multiplexed data packets. A total amount of bandwidth needed for the flight simulation can be predicted based upon, at least in part, the multiplexed data packets.

First claim

What is claimed is:

1 . A computer-implemented method comprising:
identifying, by a computing device, a plurality of information associated with a flight simulation; constructing a plurality of frame arrivals based upon, at least in part, the plurality of information associated with the flight simulation; packetizing the plurality of frame arrivals into a plurality of data packets; multiplexing the plurality of data packets to generate multiplexed data packets; and predicting a total amount of bandwidth needed for the flight simulation based upon, at least in part, the multiplexed data packets.

2 . The computer-implemented method of claim 1 , wherein the plurality of information associated with the flight simulation includes one or more aviation data containers, phases of flight, data rates for each aviation data container per format, word geometry, input window size time, or combinations thereof.

3 . The computer-implemented method of claim 1 , wherein each frame arrival of the plurality of frame arrivals is constructed per input window size time.

4 . The computer-implemented method of claim 3 further comprising determining that one of the plurality of frame arrivals does not entirely fit in an input window size time.

5 . The computer-implemented method of claim 4 further comprising sending the one of the plurality of frame arrivals that does not entirely fit in the input window size time in a next input window size time.

6 . The computer-implemented method of claim 1 , wherein the total amount of bandwidth needed for the flight simulation includes an overall raw data, an overall data, an overhead data, a filled data, or combinations thereof.

7 . The computer-implemented method of claim 1 further comprising:
optimizing at least a portion of the plurality of information associated with the flight simulation; and
using at least the portion of the plurality of information associated with the flight simulation after optimization as hardware configuration files.

8 . A computer program product residing on a computer readable storage medium having a plurality of instructions stored thereon which, when executed across one or more processors, causes at least a portion of the one or more processors to perform operations comprising:
identifying, by a computing device, a plurality of information associated with a flight simulation; constructing a plurality of frame arrivals based upon, at least in part, the plurality of information associated with the flight simulation; packetizing the plurality of frame arrivals into a plurality of data packets; multiplexing the plurality of data packets to generate multiplexed data packets; and predicting a total amount of bandwidth needed for the flight simulation based upon, at least in part, the multiplexed data packets.

9 . The computer program product of claim 8 , wherein the plurality of information associated with the flight simulation includes one or more aviation data containers, phases of flight, data rates for each aviation data container per format, word geometry, input window size time, or combinations thereof.

10 . The computer program product of claim 8 , wherein each frame arrival of the plurality of frame arrivals is constructed per input window size time.

11 . The computer program product of claim 10 , wherein the operations further comprise that one of the plurality of frame arrivals does not entirely fit in an input window size time.

12 . The computer program product of claim 11 , wherein the operations further comprise sending the one of the plurality of frame arrivals that does not entirely fit in the input window size time in a next input window size time.

13 . The computer program product of claim 8 , wherein the total amount of bandwidth needed for the flight simulation includes an overall raw data, an overall data, an overhead data, a filled data, or combinations thereof.

14 . The computer program product of claim 8 , wherein the operations further comprise:
optimizing at least a portion of the plurality of information associated with the flight simulation; and using at least the portion of the plurality of information associated with the flight simulation after optimization as hardware configuration files.

15 . A computing system including one or more processors and one or more memories configured to perform operations comprising:
identifying, by a computing device, a plurality of information associated with a flight simulation; constructing a plurality of frame arrivals based upon, at least in part, the plurality of information associated with the flight simulation; packetizing the plurality of frame arrivals into a plurality of data packets; multiplexing the plurality of data packets to generate multiplexed data packets; and predicting a total amount of bandwidth needed for the flight simulation based upon, at least in part, the multiplexed data packets.

16 . The computing system of claim 15 , wherein the plurality of information associated with the flight simulation includes one or more aviation data containers, phases of flight, data rates for each aviation data container per format, word geometry, input window size time, or combinations thereof.

17 . The computing system of claim 15 , wherein each frame arrival of the plurality of frame arrivals is constructed per input window size time.

18 . The computing system of claim 17 , wherein the operations further comprise that one of the plurality of frame arrivals does not entirely fit in an input window size time.

19 . The computing system of claim 18 , wherein the operations further comprise sending the one of the plurality of frame arrivals that does not entirely fit in the input window size time in a next input window size time.

20 . The computing system of claim 15 . wherein the operations further comprise:
optimizing at least a portion of the plurality of information associated with the flight simulation; and using at least the portion of the plurality of information associated with the flight simulation after optimization as hardware configuration files.

Assignees

• Boeing Co

Inventors

• Liaghati Amir Leon
• Delmonico Eric B
• Muwonge Charles

Classifications

• G06F9/505

  considering the load · CPC title

• G06F3/147

  using display panels · CPC title

• G09G2380/12

  Avionics applications · CPC title

• G09G2350/00

  Solving problems of bandwidth in display systems · CPC title

• G06Q50/40

  Business processes related to the transportation industry (shipping G06Q10/083) · CPC title