Resonator Optical Gyroscope Polarization Control for Bias Error

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Solution Overview

Problem

Resonator optical gyroscopes face bias errors due to the existence of parasitic modes (TE and TM) that have different effective indices of refraction and temperature coefficients, which are difficult to compensate for.

Innovation Solution

The use of at least two polarizing beam splitters (PBS) to suppress the energy of parasitic modes more than the desired modes, combined with a travelling wave resonator system that propagates optical signals in one direction, and a beat detector to determine rotation rate by adjusting carrier frequencies to resonate with the resonator.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single electromagnetic mode (TE or TM) is used in the resonator optical gyroscope, then the device complexity is reduced, but bias error increases due to the existence of parasitic modes with different effective indices of refraction and temperature coefficients

Engineering Contradiction:
Improvemode control complexityVSAvoidrotation rate measurement accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The patent extracts and removes the parasitic electromagnetic mode from the system by using a polarizing beam splitter to separate the desired mode from the parasitic mode. This extraction principle eliminates the source of bias error while maintaining system simplicity, resolving the contradiction between device complexity and measurement precision

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent introduces a polarizing beam splitter as an intermediary component between the optical source and the resonator. This mediator selectively transmits the desired electromagnetic mode while blocking the parasitic mode, thereby improving measurement precision without significantly increasing device complexity

Inventive Principle:
Principle #24Intermediary (Mediator)

2Device complexity

If parasitic modes are allowed to exist in the resonator optical gyroscope, then the device complexity remains low, but bias error occurs that is difficult to compensate for due to variations in effective indices of refraction and temperature coefficients

Engineering Contradiction:
Improvemode suppression structureVSAvoidoutput stability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The polarizing beam splitter extracts the parasitic mode from the optical path before it can enter the resonator. By removing the harmful parasitic mode at the source, the system achieves reliable and stable output without requiring complex compensation mechanisms for temperature and stress variations

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent applies preliminary anti-action by using the polarizing beam splitter to prevent the parasitic mode from entering the resonator in the first place. This preventive measure eliminates bias error before it can occur, ensuring output stability without adding complex real-time compensation systems

Inventive Principle:
Principle #9Preliminary anti-action

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

Significantly reduces bias errors in resonator optical gyroscopes by effectively suppressing parasitic modes, enhancing accuracy and reliability.

Implementation Method 1

at least two polarizing beam splitters (PBS) to suppress the energy of parasitic modes more than the desired modes

Methodology Applied
Scientific EffectPolarization: Polarisation

Implementation Method 2

adjusting a carrier frequency of the CW optical signal emitted from the optical source to equal a resonant frequency of the travelling wave resonator in a CW direction

Methodology Applied
Scientific EffectResonance: Resonance

Implementation Method 3

determining a rate of rotation of the resonator optical gyroscope around a center axis of the travelling wave resonator

Methodology Applied
Scientific EffectSagnac effect: Sagnac Effect

Data Source

PatentEP4414659B1Resonator optical gyroscope with diminished bias error
Publication Date: 2025.12.31 HONEYWELL INTERNATIONAL INC
  • EP4414659B1 patent drawingFigure 1A
  • EP4414659B1 patent drawingFigure 1B
  • EP4414659B1 patent drawingFigure 1C~1D

AI summary

Techniques are provided for diminishing bias error, in a resonator optical gyroscope, due to an undesired, parasitic optical mode which is orthogonal to a desired optical mode. Energy levels of the undesired, parasitic mode can be diminished utilizing polarizing beam splitters each of which suppresses energy of the undesired, parasitic mode of a clockwise or a counterclockwise optical signal more than energy of the desired mode of the CW optical signal. Optionally, one or more components of a travelling wave resonator system are configured to suppress energy of the undesired, parasitic mode of a clockwise and/or a counterclockwise optical signal more than energy of the desired mode of the respective optical signal(s). Optionally, the desired optical mode is either a transverse magnetic (TM) mode or a transverse electric (TE) mode, and the undesired, parasitic optical mode is respectively the TE mode or the TM mode.