Dual-Frequency IFOG Rate Computation for Drift Correction

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Solution Overview

Problem

Interferometric fiber optic gyros (IFOGs) face drift-related errors and performance degradation issues over time, requiring frequent recalibration, especially when events like fiber optic coil darkening occur.

Innovation Solution

A method and system that supply an optical input to an IFOG at two different frequencies, detect the responses, and compute the gyro rate as a function of the difference between these responses and a correction term, allowing for continuous operation without recalibration by accounting for time-dependent errors.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Duration of action of stationary object

If the IFOG operates continuously over time, then the gyro rate measurement is maintained, but drift-related errors grow and performance degrades requiring recalibration

Engineering Contradiction:
Improvecontinuous operation timeVSAvoidmeasurement accuracy
Core Design Contradiction:
Duration of action of stationary objectVSReliability

Solution Approach 1:

The patent applies periodic frequency switching between two optical frequencies (first frequency and second frequency) to the IFOG system. By alternately modulating the light source at these two frequencies and comparing the phase differences, the system periodically corrects drift errors without requiring full recalibration, thus maintaining measurement accuracy over extended operational periods.

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The patent changes the operating parameter by using two different optical frequencies instead of a single frequency. This parameter change enables the system to distinguish between Sagnac effect signals and drift errors, allowing continuous operation with maintained accuracy through differential measurement techniques.

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If recalibration is performed frequently to maintain accuracy, then measurement precision is improved, but operational time and productivity are reduced

Engineering Contradiction:
Improvegyro rate accuracyVSAvoidoperational continuity
Core Design Contradiction:
Measurement precisionVSProductivity

Solution Approach 1:

The patent implements a self-correcting mechanism where the IFOG system automatically compensates for its own drift errors by comparing measurements taken at two different frequencies. The system uses the difference in phase responses at these frequencies to calculate and correct drift-related errors, eliminating the need for external recalibration operations and maintaining continuous productivity.

Inventive Principle:
Principle #25Self-service

3Duration of action of stationary object

If the fiber optic coil darkens due to degradation events, then the IFOG performance degrades, but the system continues operating without immediate failure

Engineering Contradiction:
Improveoperation continuityVSAvoidresponse sensitivity
Core Design Contradiction:
Duration of action of stationary objectVSMeasurement precision

Solution Approach 1:

When fiber optic coil darkening occurs, the patent compensates by changing the measurement parameter from single-frequency to dual-frequency operation. The system measures phase differences at two frequencies and uses the differential signal to correct for intensity variations caused by darkening, maintaining measurement precision despite the degradation event.

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables stable computation of the gyro rate without recalibration, even during performance degradation events, by using the difference in responses at two frequencies and pre-computed scale factors, thereby reducing the need for frequent recalibration and maintaining accurate navigation data.

Implementation Method 1

an interferometric fiber optic gyro (IFOG)... detecting a difference in responses of the IFOG to the optical input at the first and second frequencies... computing a gyro rate

Methodology Applied
Scientific EffectSagnac effect: Sagnac Effect

Data Source

PatentUS10502585B2Gyro rate computation for an interferometric fiber optic gyro
Publication Date: 2019.12.10 THE BOEING CO
  • US10502585B2 patent drawing
  • US10502585B2 patent drawing
  • US10502585B2 patent drawing

AI summary

A method comprises supplying an optical input to an interferometric fiber optic gyro (IFOG) at a first frequency and then a different second frequency; detecting a difference in responses of the IFOG to the optical input at the first and second frequencies; and computing a gyro rate as a function of the difference and a correction term.