Assessing aircraft interference path loss employing discrete frequency stirring

Patent metadata

Field	Value
Publication number	US-9762335-B2
Application number	US-201313924609-A
Country	US
Kind code	B2
Filing date	Jun 23, 2013
Priority date	Jul 16, 2008
Publication date	Sep 12, 2017
Grant date	Sep 12, 2017

Abstract

A method for accessing aircraft interference path loss in an aircraft. A plurality of radio frequency signals that are stepped through a plurality of frequencies in a frequency range is transmitted from a plurality of locations within an interior of the aircraft. Radio frequency signals present at a receive antenna are received in response to transmitting the plurality of radio frequency signals to form a plurality of measurements. An average of averages curve is generated from the plurality of measurements. A peak to average ratio is identified. Field uniformity is identified. A standard error for the average of averages curve is determined. An upper bound for the aircraft interference path loss in the aircraft is predicted using the average of averages curve, the peak to average ration, the field uniformity, and the standard error.

First claim

What is claimed is:

1. A method for identifying attenuation within a structure, the method comprising:
transmitting a plurality of electromagnetic signals that are stepped through a plurality of frequencies in a frequency range from a plurality of locations within the structure,
measuring electromagnetic signals received at a receiver on the exterior of the structure in response to transmitting the plurality of electromagnetic signals to form a plurality of measurements;
performing a statistical analysis using the plurality of measurements to form a result;
predicting a set of attenuations for the structure using the result;
calculating a sample independence of the electromagnetic signals by calculating a value representing a degree to which data representing the electromagnetic signals is correlated; and
responsive to a determination that the value is greater than about zero, at least one of increasing a step size of the plurality of frequencies and sifting the data to obtain an uncorrelated data set, and then re-performing transmitting, measuring, performing, and predicting.

2. The method of claim 1 , wherein the transmitting step comprises:
broadcasting a radio frequency signal at a frequency from a location within the plurality of locations;
incrementing the frequency by the step size to form a new frequency within the plurality of frequencies;
transmitting a new radio frequency signal from the location at the new frequency within the plurality of locations;
repeating the incrementing and transmitting step until the plurality of frequencies has been used to transmit the new radio frequency signal; and
repeating the broadcasting, incrementing, transmitting, and repeating steps for each location within the plurality of locations.

3. The method of claim 1 , wherein the performing step comprises:
generating an average of averages curve from the plurality of measurements;
identifying a peak to average ratio;
identifying field uniformity;
determining a standard error for the average of averages curve; and
predicting the set of attenuations for the structure using the average of averages curve, the peak to average ratio, the field uniformity, and the standard error.

4. The method of claim 3 , wherein the step of identifying the peak to average ratio comprises:
calculating a difference between the average of averages curve and an average of peaks curve.

5. The method of claim 3 further comprising:
identifying a standard deviation from average values of signal strength, wherein the standard deviation is used to identify the field uniformity.

6. The method of claim 1 , wherein the predicting step comprises:
identifying a path from a location within the plurality of locations to a receive antenna, wherein the path has a largest amount of attenuation.

7. The method of claim 1 , wherein the predicting step comprises:
identifying a path from a location within the plurality of locations to a receive antenna, wherein the path has a smallest amount of attenuation.

8. The method of claim 1 wherein the plurality of locations within the structure comprises at least two of the group consisting of a flight deck, a main cabin, a galley, a cargo hold, and an upstairs cabin.

9. The method of claim 8 , wherein the step of identifying the test setup for the structure prior to transmitting the plurality of frequencies comprises:
identifying a set of zones for the structure;
identifying a set of test locations within the set of zones;
identifying a set of transmit antennas;
identifying a set of frequency ranges; and
identifying the step size for each frequency range.

10. The method of claim 1 , wherein the structure is selected from one of a building, an aircraft, a submarine, a spacecraft, and a ship.

11. The method of claim 1 , wherein the step size is identified based on an estimate of a resident mode bandwidth.

12. The method of claim 1 , wherein the value is calculated using Pearson's “R” auto correlation check.

13. The method of claim 1 further comprising:
calculating a sample independence of the electromagnetic signals by calculating a value representing a degree to which data representing the electromagnetic signals is correlated.

14. The method of claim 13 , wherein the value is calculated using Pearson's “R” auto correlation check.

Assignees

• Boeing Co

Inventors

• Horton Nathaniel Thomas
• Kirchoff Kenneth Patrick
• Lewis Dennis Michael

Classifications

• H04B17/297

  Self-testing arrangements · CPC title

• H04B17/345

  Interference values ({signal-to-interference ratio [SIR] or carrier-to-interference ratio [CIR]} H04B17/336) · CPC title

• H04B17/26

  using historical data, averaging values or statistics · CPC title

• H04B7/18506

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

• H04B17/373 Primary

  Predicting channel quality {or other radio frequency [RF]} parameters · CPC title