GNSS RFI Sigma Averaging for Faster Satellite Readmittance

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Solution Overview

Problem

Global navigation satellite system (GNSS) receivers experience accuracy issues due to broadband radio frequency interference (RFI), leading to exclusion of satellite measurements from differential correction data and integrity monitoring, requiring a method to quickly and reliably readmit these measurements when interference decreases.

Innovation Solution

A method involving the calculation of first and second RFI-based averaged sigmas, where the first sigma includes the excluded measurement and the second sigma does not, allowing readmission when the first sigma is less than or equal to the second, facilitating quicker reacceptance into differential corrections and integrity monitors.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If satellite measurements are excluded from differential correction data and integrity monitors when C/N0 drops below threshold due to RFI, then measurement reliability is improved, but system productivity and positional accuracy deteriorate due to loss of available measurements

Engineering Contradiction:
Improvemeasurement reliabilityVSAvoidsystem productivity
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent implements dynamic readmittance criteria that adapt to current signal conditions. Instead of permanently excluding satellite measurements when C/N0 drops below threshold, the system continuously monitors signal quality and allows readmittance when conditions improve, creating a dynamic rather than static exclusion approach that optimizes both reliability and productivity

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system employs feedback mechanisms by continuously monitoring C/N0 values and using this information to control the readmittance decision process. The readmittance criteria are based on feedback from signal quality measurements, allowing the system to adjust its behavior based on current RFI conditions and restore measurements when appropriate

Inventive Principle:
Principle #23Feedback

2Reliability

If satellite measurements are excluded during RFI events, then integrity monitor reliability is improved, but time loss and system downtime increase

Engineering Contradiction:
Improveintegrity monitor reliabilityVSAvoidsystem downtime
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent establishes predetermined readmittance criteria before RFI events occur. These criteria, based on C/N0 thresholds and signal quality metrics, are prepared in advance to enable rapid readmittance decisions when interference subsides, reducing the time loss associated with reevaluating readmittance conditions after an event

Inventive Principle:
Principle #10Preliminary action

3Productivity

If excluded satellite measurements are quickly readmitted when C/N0 improves, then system availability is improved, but risk of reaccepting corrupted measurements increases

Engineering Contradiction:
Improvesystem availabilityVSAvoidmeasurement integrity
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system uses continuous feedback from C/N0 monitoring to control the readmittance process. Rather than immediately readmitting measurements when C/N0 first exceeds the threshold, the system uses the feedback signal to verify sustained improvement in signal quality, ensuring that readings are not reaccepted during ongoing interference events

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent introduces an intermediary readmittance evaluation process between the exclusion decision and the actual readmittance of measurements. This intermediary step evaluates multiple criteria including C/N0 thresholds and signal stability to mediate the transition from excluded to accepted status, preventing premature readmittance of corrupted data

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentEP3012665B1Systems and methods for averaging satellite sigmas and readmitting excluded satellite measurements into differential corrections and integrity monitors
Publication Date: 2019.08.14 HONEYWELL INTERNATIONAL INC
  • EP3012665B1 patent drawingFigure 1
  • EP3012665B1 patent drawingFigure 2
  • EP3012665B1 patent drawing

AI summary

Systems and methods for averaging satellite sigmas and readmitting excluded satellite measurements into differential corrections and integrity monitors are provided. In one embodiment, a method comprises: calculating a first RFI based averaged sigma and a second RFI based averaged sigma, wherein the first RFI based averaged sigma includes a sigma for the excluded satellite measurement and wherein the second RFI based averaged sigma does not include the sigma for the excluded satellite measurement; and, readmitting the excluded satellite measurement into either a differential correction broadcast or a respective integrity monitor when the first RFI based averaged sigma is less than or equal to the second RFI based averaged sigma.