Atom Beam Gyroscope Magnetic Field Gradient Zeeman Effect

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Solution Overview

Problem

Current gyroscope systems face challenges in accurately measuring rotation angles due to limitations in detecting subtle changes in Doppler shifts and Zeeman effects, particularly in avionic applications where precision is crucial.

Innovation Solution

An atom beam gyroscope system utilizing a magneto-optical trap or evaporated alkali metal beam cell, combined with a detection system featuring a circularly-polarized detection laser and magnetic field gradient, measures rotation by detecting changes in optical energy absorption of alkali metal atoms through Doppler- and Zeeman-shifts, allowing for precise calculation of rotation angles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If conventional Doppler shift detection methods are used, then the system structure remains simple, but the measurement precision of rotation angles deteriorates due to inability to detect subtle changes

Engineering Contradiction:
Improverotation angle measurement precisionVSAvoiddetection system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent introduces an intermediary magnetic field gradient that couples the rotation-induced Doppler shift to a measurable Zeeman effect. The magnetic field gradient acts as a mediator that amplifies the subtle Doppler shift changes into detectable absorption changes, allowing precise rotation angle measurement without directly detecting the tiny Doppler shifts themselves.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent changes the measurement parameter from direct Doppler shift frequency detection to optical absorption intensity detection under a magnetic field gradient. By transforming the measurement into detecting absorption changes rather than frequency shifts, the system achieves higher precision with simpler detection equipment.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If direct Doppler shift detection is used, then the device complexity remains low, but the reliability of rotation measurement deteriorates due to insufficient sensitivity

Engineering Contradiction:
Improverotation measurement reliabilityVSAvoiddetection system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The magnetic field gradient serves as a reliable intermediary that converts subtle rotation-induced Doppler shifts into pronounced Zeeman absorption changes. This intermediary mechanism significantly enhances measurement reliability by making the detection signal much stronger and less susceptible to noise, while avoiding the need for complex direct frequency shift detection systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Measurement precision

If subtle Doppler shift changes are directly detected, then measurement precision could improve, but the difficulty of detecting and measuring increases significantly

Engineering Contradiction:
Improverotation angle measurement precisionVSAvoidDoppler shift detection difficulty
Core Design Contradiction:
Measurement precisionVSDifficulty of detecting and measuring

Solution Approach 1:

The patent eliminates the difficulty of direct subtle Doppler shift detection by introducing the magnetic field gradient intermediary. The Zeeman effect under the gradient converts the hard-to-detect frequency shifts into easy-to-detect absorption intensity changes, maintaining high measurement precision while dramatically reducing detection difficulty.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent changes the detection parameter from frequency shift (difficult to measure precisely) to absorption intensity (easy to measure with high precision). This parameter transformation maintains the sensitivity needed for precise rotation measurement while using simpler, more reliable detection methods.

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

The system achieves high precision in calculating rotation angles by effectively detecting slight deviations in alkali metal atom absorption, overcoming limitations in existing technologies and providing accurate navigation data for aircraft and spacecraft.

Implementation Method 1

a magnetic field generator configured to generate a magnetic field gradient that increases from a nominal axis of the atom beam, such that the magnetic field gradient and the circularly-polarized detection beam can substantially adjust a probability of absorption of photons of the detection beam by alkali metal atoms having a non-zero velocity relative to the detection beam due to the Zeeman effect

Methodology Applied
Scientific EffectZeeman effect: Zeeman Effect

Implementation Method 2

an amount of Doppler-shift of the atom beam resulting from rotation of the gyroscope system about the sensitive axis can be detected by the photodetector

Methodology Applied
Scientific EffectDoppler-shift: Doppler Effect

Data Source

PatentEP3336586B1Atom beam gyroscope
Publication Date: 2020.06.17 NORTHROP GRUMMAN GUIDANCE AND ELECTRONICS CO INC
  • EP3336586B1 patent drawingFigure 1~2
  • EP3336586B1 patent drawingFigure 3~4
  • EP3336586B1 patent drawingFigure 5~6

AI summary

An atom beam gyroscope system is provided. The system comprises: an atom beam system configured to generate a first atom beam and a second atom beam, the first and second atom beams comprising alkali metal atoms; a detection system comprising a first detection laser, a second detection laser, a first photodetector, and a second photodetector, the first detection laser being configured to generate a first optical detection beam, the second detection laser being configured to generate a second optical detection beam, the first photodetector being configured to measure an intensity of the first optical detection beam and to generate a first intensity signal and the second photodetector being configured to measure an intensity of the second optical detection beam and to generate a second intensity signal; and a gyroscope sensor configured to calculate rotation and linear acceleration of the atom beam gyroscope system.