Variable Time Constant Filter for Gyroscope Control Loops

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Solution Overview

Problem

High performance Coriolis gyroscope sensors with vibrating structures, such as MEMS, face challenges due to variable Q-factors and temperature variations, leading to inconsistent frequency responses, particularly at low frequencies, which are problematic for high performance and dynamic systems.

Innovation Solution

A method using an electronic control system with a filter having a variable time constant, which adapts to the estimated characteristics of the vibrating structure, such as frequency, Q-factor, or temperature, to optimize the time constant and enhance the measurement of rotation rates.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a fixed time constant filter is used in the control loop, then the device complexity is reduced, but the measurement precision deteriorates due to low frequency gain variations

Engineering Contradiction:
Improvefilter configurationVSAvoidlow frequency gain consistency
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The patent applies the dynamics principle by making the filter time constant variable rather than fixed. The time constant is dynamically adjusted based on the measured Q-factor of the vibrating structure, allowing the filter to adapt to changing system characteristics and maintain consistent low frequency gain response across different operating conditions.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent implements feedback by continuously measuring the Q-factor of the vibrating structure and using this information to adjust the filter time constant. This closed-loop approach ensures that the filter remains optimized for the current system state, preventing low frequency gain variations while maintaining measurement precision.

Inventive Principle:
Principle #23Feedback

2Adaptability or versatility

If the Q-factor of the vibrating structure varies due to manufacturing tolerances and temperature, then the adaptability of the system to different conditions is improved, but the frequency response consistency deteriorates

Engineering Contradiction:
ImproveQ-factor variation toleranceVSAvoidfrequency response consistency
Core Design Contradiction:
Adaptability or versatilityVSStability of the object's composition

Solution Approach 1:

The system uses feedback by measuring the actual Q-factor and using this information to adjust the filter time constant, thereby maintaining consistent frequency response despite Q-factor variations from manufacturing tolerances or temperature changes.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent applies parameter changes by adjusting the filter time constant based on the measured Q-factor. This dynamic parameter adjustment compensates for Q-factor variations and maintains consistent frequency response characteristics across different operating conditions.

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If pole-zero cancellation is used to shape the frequency response, then the frequency response shaping capability is improved, but the measurement precision at low frequencies deteriorates due to inconsistent responses

Engineering Contradiction:
Improvefrequency response shapingVSAvoidlow frequency response consistency
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The patent replaces the mechanical pole-zero cancellation approach with an electronic filtering solution. By using a filter with a time constant adjusted based on the measured Q-factor, the system achieves frequency response shaping without the low frequency inconsistencies associated with pole-zero cancellation.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS10753745B2Gyroscope loop filter
Publication Date: 2020.08.25 ATLANTIC INERTIAL SYST LTD
  • US10753745B2 patent drawing
  • US10753745B2 patent drawing
  • US10753745B2 patent drawing

AI summary

There is provided a method of sensing a rotation rate using a vibrating structure gyroscope, said gyroscope comprising an electronic control system comprising one or more control loops, wherein at least one of said control loops comprises a filter having a variable time constant, said method comprising the steps of: determining or estimating a characteristic of the vibrating structure of said gyroscope; and adapting or varying said time constant of said filter with the determined or estimated characteristic of said vibrating structure.