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US11226203B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11226203-B2
Application numberUS-201816497627-A
CountryUS
Kind codeB2
Filing dateMar 28, 2018
Priority dateMar 31, 2017
Publication dateJan 18, 2022
Grant dateJan 18, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

This disclosure relates to an underground mining vehicle comprising a three-axis MEMS gyroscope rotatable about a rotation axis and a gyroscope interface that calculates a first rotation rate bias with respect to a first axis different to the rotation axis, a second rotation rate bias with respect to a second axis different to the first axis and different to the rotation axis, a rotation rate about the rotation axis based on the Earth rotation rate vector by correcting the rotational measurement data using the first rotation rate bias and the second rotation rate bias and a third rotation rate bias with respect to the rotation axis based on the calculated rotation rate about the rotation axis. A navigation unit receives the first rotation rate bias, the second rotation rate bias and the third rotation rate bias and calculates a pose of the vehicle.

First claim

Opening claim text (preview).

The invention claimed is: 1. An underground mining vehicle, comprising: a three-axis MEMS gyroscope mounted in a fixed position and pose relative to the underground mining vehicle and mounted on a rotator having a single rotation axis configured to index the three axis MEMS gyroscope about the rotation axis into multiple different orientations; a gyroscope interface connected to the three-axis MEMS gyroscope configured to receive rotational measurement data from the three-axis MEMS gyroscope for the multiple different orientations and further configured to: in a first step: calculate a first rotation rate bias of the three-axis MEMS gyroscope with respect to a first axis substantially orthogonal to the rotation axis based on the rotational measurement data, calculate a second rotation rate bias of the three-axis MEMS gyroscope with respect to a second axis substantially orthogonal to the first axis and to the rotation axis based on the rotational measurement data, calculate a corrected first rotation rate by correcting the rotational measurement data using the first rotation rate bias; calculate a corrected second rotation rate by correcting the rotational measurement data using the second rotation rate bias; in a second step after the first step: calculate an expected rotation rate about the rotation axis by performing an arithmetic operation on the Earth rotation rate vector, known for a given location of the underground mining vehicle, the corrected first rotation rate and the corrected second rotation rate; and in a third step after the second step: calculate a third rotation rate bias of the three-axis MEMS gyroscope with respect to the rotation axis based on the calculated expected rotation rate about the rotation axis; and a navigation unit connected to the gyroscope interface configured to receive the first rotation rate bias, the second rotation rate bias and the third rotation rate bias from the gyroscope interface, and calculate a pose of the underground mining vehicle based on the Earth rotation rate vector, the first rotation rate bias, second rotation rate bias and third rotation rate bias. 2. The underground mining vehicle of claim 1 , further comprising a vehicle controller connected to the vehicle and configured to stop the vehicle; correct an inertial navigation system while the vehicle is stopped; cause the rotator to rotate the three-axis gyroscope while the vehicle is stopped; cause the gyroscope interface to calculate the first, second and third rotation rate biases; and resume movement of the vehicle based on the calculated pose. 3. The underground mining vehicle of claim 1 , further comprising a three-axis accelerometer communicatively coupled to the navigation unit, wherein the navigation unit is configured to calculate the pose based on acceleration data from the three-axis accelerometer. 4. The underground mining vehicle of claim 1 , wherein the navigation unit is an inertial navigation unit and is configured to determine an absolute location of the underground mining vehicle based on the pose. 5. The underground mining vehicle of claim 1 , wherein the gyroscope interface is configured to calculate the expected rotation rate ω third about the rotation axis according to ω third =√{square root over (ω Earth 2 −ω first 2 −ω second 2 )} where ω Earth is the Earth rotation rate vector magnitude, ω first is the corrected first rotation rate about the first axis and ω second is the corrected second rotation rate about the second axis corrected by the calculated first and second rotation rate bias, respectively. 6. The underground mining vehicle of claim 1 , further comprising a filter connected to the gyroscope interface and configured to continually track the third rotation rate bias. 7. The underground mining vehicle of claim 1 , further comprising a further three-axis MEMS gyroscope mounted in a fixed position and pose relative to the underground mining vehicle, wherein the navigation unit is connected to the further three-axis MEMS gyroscope and is configured to receive further rotational measurement data from the further three-axis MEMS gyroscope and to calculate the pose of the underground mining vehicle based on the further rotational measurement data. 8. The underground mining vehicle of claim 1 , wherein the gyroscope interface is configured to calculate the expected rotation rate ω third about the rotation axis according to ω third =√{square root over (ω Earth 2 −ω first 2 −ω second 2 )}, where ω Earth is the Earth rotation rate vector magnitude, ω first is the corrected first rotation rate about the first axis and ω second is corrected second rotation rate about the second axis corrected by the calculated first and second rotation rate bias, respectively; the underground mining vehicle further comprises a three-directional accelerometer communicatively coupled to the navigation unit and the navigation unit is configured to calculate the pose based on acceleration data from the three-directional accelerometer; and the underground mining vehicle further comprises a further three-axis MEMS gyroscope mounted in a fixed position and pose relative to the underground mining vehicle and the navigation unit is connected to the further three-axis MEMS gyroscope and is configured to receive further rotational measurement data from the further three-axis MEMS gyroscope and to calculate the pose of the underground mining vehicle based on the further rotational measurement data. 9. A method for calculating a pose of an underground mining vehicle, the method comprising: indexing a three axis MEMS gyroscope mounted in a fixed position and pose relative to the underground mining vehicle about a single rotation axis into multiple different orientations; receiving rotational measurement data from the three-axis MEMS gyroscope for the multiple different orientations; in a first step: calculating a first rotation rate bias of the three-axis MEMS gyroscope with respect to a first axis substantially orthogonal to the rotation axis based on the rotational measurement data; calculating a second rotation rate bias of the three-axis MEMS gyroscope with respect to a second axis substantially orthogonal to the first axis and different to the rotation axis based on the rotational measurement data, calculating a corrected first rotation rate by correcting the rotational measurement data using the first rotation rate bias; calculating a corrected second rotation rate by correcting the rotational measurement data using the second rotation rate bias; in a second step after the first step: calculating an expected rotation rate about the rotation axis by performing an arithmetic operation on the Earth rotation rate vector, known for a given location of the underground mining vehicle, the corrected first rotation rate and the corrected second rotation rate; and in a third step after the second step: calculating a third rotation rate bias of the three-axis MEMS gyroscope with respect to the rotation axis based on the calculated expected rotation rate about the rotation axis; and calculating a pose of the underground mining vehicle based on the Earth rotation rate vector, the first rotation rate bias, second rotation rate bias and third rotation rate bias. 10. The method of claim 9 , further comprising: stopping the vehicle; correcting an inertial navigation system while the vehicle is stopped; rotating the three-axis gyroscope while the vehicle is stopped; calculating the first, second and third rotation rate biases; and resuming movement of the vehicle based on the calculated pose. 11. The method of claim 10 , wherein stopping t

Assignees

Inventors

Classifications

  • for gravity · CPC title

  • G01C21/188Primary

    for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems · CPC title

  • G01C21/20Primary

    Instruments for performing navigational calculations (G01C21/24, G01C21/26 take precedence) · CPC title

  • containing distinct electrical or optical devices of particular relevance for their function, e.g. microelectro-mechanical systems [MEMS] (B81B7/04 takes precedence) · CPC title

  • Stabilised platforms, e.g. by gyroscope · CPC title

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What does patent US11226203B2 cover?
This disclosure relates to an underground mining vehicle comprising a three-axis MEMS gyroscope rotatable about a rotation axis and a gyroscope interface that calculates a first rotation rate bias with respect to a first axis different to the rotation axis, a second rotation rate bias with respect to a second axis different to the first axis and different to the rotation axis, a rotation rate a…
Who is the assignee on this patent?
Commw Scient Ind Res Org
What technology area does this patent fall under?
Primary CPC classification G01C21/188. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Jan 18 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).