Cold-Atom Gyrometer Bias Correction via Dual-Sensor Interferometry

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Solution Overview

Problem

Existing inertial sensors face challenges in accurately measuring rotational velocities due to measurement biases and errors, which affect the precision and reliability of inertial navigation systems.

Innovation Solution

The development of an interferometric inertial ultracold-atom sensor with a dual-sensor configuration on an atom chip, where two elementary sensors with identical paths but opposite directions are used to simultaneously measure phases, allowing for the elimination of measurement biases by calculating the difference between the phases measured by each sensor.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a single cold-atom sensor is used to measure rotational velocity, then the device complexity is low, but measurement precision deteriorates due to unavoidable biases

Engineering Contradiction:
Improverotational velocity measurement precisionVSAvoidsensor configuration complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The invention divides a single sensor into two elementary sensors that share common components (waveguides, conductive elements, atom generation device) but operate with opposite path directions. This segmentation allows independent phase measurements that can be differential processed to eliminate biases, improving measurement precision while controlling complexity through component sharing

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention creates a copy of the measurement path with reverse direction for the second elementary sensor. This mirrored configuration enables the system to measure the same physical quantity (rotational velocity) through two complementary paths, where the difference between measurements cancels out systematic biases

Inventive Principle:
Principle #26Copying

2Measurement precision

If measurement paths are made longer to improve sensitivity, then the gyrometer sensitivity improves, but measurement time increases

Engineering Contradiction:
Improvegyrometer sensitivityVSAvoidmeasurement cycle time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The invention enables continuous measurement by having two elementary sensors operate simultaneously in opposite directions. While one sensor completes its measurement cycle, the other is already underway, allowing the system to maintain continuous phase difference measurement without waiting for individual long paths to complete, thus preserving sensitivity while reducing effective measurement time

Inventive Principle:
Principle #20Continuity of useful action

Solution Approach 2:

The invention uses periodic modulation of the atom paths where atoms traverse the measurement paths in alternating sequences. This periodic action allows the system to accumulate phase information over extended effective path lengths while maintaining a continuous measurement rhythm that prevents time loss

Inventive Principle:
Principle #19Periodic 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

This approach significantly reduces measurement uncertainty and improves the sensitivity of the gyrometer, enabling longer inertial navigation times with enhanced accuracy and reliability.

Implementation Method 1

A term dependent on the Sagnac effect, and therefore on velocity of rotation, is thus added to the energy difference between the two states

Methodology Applied
Scientific EffectSagnac effect: Sagnac Effect

Implementation Method 2

Operation of cold-atom gyrometers is based on interferometry, and measuring the phase difference of the interferometer allows a measurement of rotation to be obtained

Methodology Applied
Scientific EffectInterference: Interference

Data Source

PatentUS20250044092A1Cold-atom sensor of gyrometer type with bias corrected
Publication Date: 2025.02.06 THALES SA
  • US20250044092A1 patent drawing
  • US20250044092A1 patent drawing
  • US20250044092A1 patent drawing

AI summary

An interferometric inertial ultracold-atom sensor of gyrometer type, including an atom chip comprising at least one set of a first and second elementary sensor, a power-supplying device, the magnetic-field generator and the power-supplying device being configured to apply the magnetic field, the DC currents and the microwave signals in a predetermined sequence, the arrangement of the group of one or more conductive elements of each sensor and the sequence further being configured so that the path associated with the first elementary sensor and the path associated with the second elementary sensor are identical and traced simultaneously and in inverse directions by the clouds of ultracold atoms associated with a given internal state, the sensor further comprising a detecting system.