Angle random walk minimization for frequency modulated gyroscopes

US11268810B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11268810-B2
Application numberUS-201916507453-A
CountryUS
Kind codeB2
Filing dateJul 10, 2019
Priority dateJul 10, 2019
Publication dateMar 8, 2022
Grant dateMar 8, 2022

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

Compared to amplitude modulated gyroscopes, frequency modulated (FM) gyroscopes have demonstrated excellent long-term stability. A notable limitation with FM gyroscopes is FM operation can decrease short-term stability. Short-term stability is typically quantified via angle random walk (ARW). The present disclosure provides an FM gyroscope ARW minimization method.

First claim

Opening claim text (preview).

What is claimed as new and desired to be protected by Letters Patent of the United States is: 1. A method of determining a driving signal for a dual mode resonator of a gyroscope, said method comprising: driving, via a first mode phase-locked loop (PLL) set at first mode phase, a first mode of the dual mode resonator; obtaining, via a detector, a first mode power spectral density (PSD) value of the dual mode resonator, a first mode amplitude of the dual mode resonator and a first mode frequency of the dual mode resonator based on the PLL set at the first mode phase; repeating said driving the first mode of the dual mode resonator and said obtaining a respective first mode PSD value, a respective first mode amplitude of the dual mode resonator and a respective first mode frequency of the dual mode resonator based on the PLL set at a respective first mode phase a number n times to obtain n respective first mode PSD values of the dual mode resonator, n respective first mode amplitudes of the dual mode resonator and n respective first mode frequencies of the dual mode resonator, each repetition of said driving the first mode of the dual mode resonator and said obtaining a respective first mode PSD value, a respective first mode amplitude of the dual mode resonator and a respective first mode frequency of the dual mode resonator having the first mode PLL being set at a different respective first mode phase; driving, via a second mode PLL set at second mode phase, a second mode of the dual mode resonator; obtaining, via the detector, a second mode PSD value of the dual mode resonator, a second mode amplitude of the dual mode resonator and a second mode frequency of the dual mode resonator based on the PLL set at the second mode phase; repeating said driving the second mode of the dual mode resonator and said obtaining a respective second mode PSD value, a respective second mode amplitude of the dual mode resonator and a respective second mode frequency of the dual mode resonator based on the PLL set at a respective second mode phase a number m times to obtain m respective second mode PSD values of the dual mode resonator, m respective second mode amplitudes of the dual mode resonator and m respective second mode frequencies of the dual mode resonator, each repetition of said driving the second mode of the dual mode resonator and said obtaining a respective second mode PSD value, a respective second mode amplitude of the dual mode resonator and a respective second mode frequency of the dual mode resonator having the second mode PLL being set at a different respective second mode phase; determining an angle random walk, ARW, value of the dual mode resonator using the following equation, ARW ⁡ ( deg / sec Hz ) = 360 ⁢ P 1 ⁡ ( Δ ⁢ ⁢ f ) ⁢ f s 2 + P 2 ⁡ ( Δ ⁢ ⁢ f ) ⁢ f s 2 1 2 ⁢ A g ⁡ ( a 1 a 2 + a 2 α 1 ) , wherein f s is a sampling frequency, wherein A g is the angular gain of the dual mode resonator, wherein a 1 is the first mode amplitude of the dual mode resonator based on the PLL set at the first mode phase, wherein a 2 is the second mode amplitude of the dual mode resonator based on the PLL set at the second mode phase, wherein f 1 is the first mode frequency of the dual mode resonator based on the PLL set at the first mode phase, wherein f 2 is the second mode frequency of the dual mode resonator based on the PLL set at the second mode phase, wherein Δf=|f 1 −f 2 |, wherein P 1 (Δf) is a PSD value of the first mode frequency of the dual mode resonator based on the PLL set at the first mode phase as demodulated at Δf, and wherein P 2 (Δf) is a PSD value of the second mode frequency of the dual mode resonator based on the PLL set at the second mode phase as demodulated at Δf. 2. The method of claim 1 , wherein n=m. 3. The method of claim 2 , wherein the PLL is set at the respective first mode phase the number n times between 0° and −180°. 4. The method of claim 3 , wherein the PLL is set at the respe

Assignees

Inventors

Classifications

  • the devices having two sensing masses in anti-phase motion · CPC title

  • Details of the phase-locked loop · CPC title

  • the devices involving a micromechanical structure · CPC title

  • Signal processing · CPC title

  • Signal processing not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719 · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US11268810B2 cover?
Compared to amplitude modulated gyroscopes, frequency modulated (FM) gyroscopes have demonstrated excellent long-term stability. A notable limitation with FM gyroscopes is FM operation can decrease short-term stability. Short-term stability is typically quantified via angle random walk (ARW). The present disclosure provides an FM gyroscope ARW minimization method.
Who is the assignee on this patent?
Government Of The United States As Represented By The Secretary Of The Navy, Us Navy
What technology area does this patent fall under?
Primary CPC classification G01C19/5726. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Mar 08 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 11 related publications on this page (citations in our corpus or others sharing the same primary CPC).