Geoid measurement method, geoid measurement apparatus, geoid estimation device, and geoid calculation data collection device

US11378397B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11378397-B2
Application numberUS-201917057862-A
CountryUS
Kind codeB2
Filing dateJun 4, 2019
Priority dateJul 24, 2018
Publication dateJul 5, 2022
Grant dateJul 5, 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.

A change in geoid height is measured easily. A geoid measurement method of the present invention executes an inertial measurement data acquiring step, a comparison data acquiring step, a state variable estimating step, and a geoid calculating step. In the inertial measurement data acquiring step, data related to velocity, position, and attitude angle is acquired as inertially-derived data based on the output of an inertial measurement part having a three-axis gyro and a three-axis accelerometer attached to a moving body. In the comparison data acquiring step, data related to velocity is acquired as comparison data from a source other than the inertial measurement part. In the state variable estimating step, state variables including a plumb line deviation are estimated by using the inertially-derived data and the comparison data to apply a Kalman filter in which the plumb line deviation is included in the state variables.

First claim

Opening claim text (preview).

What is claimed is: 1. A geoid measurement method comprising: an inertial measurement data acquiring step of acquiring data related to velocity, position, and attitude angle as inertially-derived data based on an output of an inertial measurement part having a three-axis gyro and a three-axis accelerometer attached to a moving body; a comparison data acquiring step of acquiring data related to velocity as comparison data from a source other than the inertial measurement part; a state variable estimating step of estimating state variables including a plumb line deviation by using the inertially-derived data and the comparison data to apply a Kalman filter in which the plumb line deviation is included in the state variables; and a geoid calculating step of calculating a change in geoid height based on the estimated plumb line deviation at an estimated position that the estimating applied to. 2. The geoid measurement method according to claim 1 , wherein the data related to velocity, position, and attitude angle acquired in the inertial measurement data acquiring step is data that is corrected using the estimated state variables. 3. The geoid measurement method according to claim 2 , wherein in the geoid calculating step, a geoid height is calculated at each of the estimated positions based on information about a geoid height at a reference position acquired in advance. 4. The geoid measurement method according to claim 1 , wherein in the geoid calculating step, a geoid height is calculated at each of the estimated positions based on information about a geoid height at a reference position acquired in advance. 5. A geoid measurement apparatus comprising: an inertial measurement data acquisition part, provided with an inertial measurement part having a three-axis gyro and a three-axis accelerometer to be attached to a moving body, and that acquires data related to velocity, position, and attitude angle as inertially-derived data; a comparison data acquisition part that acquires data related to velocity as comparison data from a source other than the inertial measurement part; a state variable estimation part that estimates state variables including a plumb line deviation by using the inertially-derived data and the comparison data to apply a Kalman filter in which the plumb line deviation is included in the state variables; and a geoid calculation part that calculates a change in geoid height based on the estimated plumb line deviation at an estimated position that the estimating applied to. 6. The geoid measurement apparatus according to claim 5 , wherein the data related to velocity, position, and attitude angle acquired by the inertial measurement data acquisition part is data that is corrected using the estimated state variable. 7. The geoid measurement apparatus according to claim 6 , further comprising: a recording part that records information about a geoid height with respect to a predetermined reference position, wherein the geoid calculation part calculates a geoid height at each of the estimated positions based on the information about the geoid height. 8. The geoid measurement apparatus according to claim 5 , further comprising: a recording part that records information about a geoid height with respect to a predetermined reference position, wherein the geoid calculation part calculates a geoid height at each of the estimated positions based on the information about the geoid height. 9. The geoid measurement apparatus according to claim 5 , wherein the comparison data acquisition part captures radio waves transmitted from an artificial satellite. 10. The geoid measurement apparatus according to claim 5 , wherein the comparison data acquisition part includes a speedometer. 11. The geoid measurement apparatus according to claim 5 , wherein the gyro is a gyro using atomic waves or ions. 12. A geoid estimation device comprising: a recording part that records inertially-derived data and comparison data in association with each other, the inertially-derived data being data related to velocity, position, and attitude angle acquired based on an output of an inertial measurement part having a three-axis gyro and a three-axis accelerometer attached to a moving body, and the comparison data being data related to velocity acquired from a source other than the inertial measurement part; a state variable estimation part that estimates state variables including a plumb line deviation by using the inertially-derived data and the comparison data to apply a Kalman filter in which the plumb line deviation is included in the state variables; and a geoid calculation part that calculates a change in geoid height based on the estimated plumb line deviation at an estimated position that the estimating applied to. 13. The geoid estimation device according to claim 12 , wherein the recording part also records information about a geoid height with respect to a predetermined reference position, and the geoid calculation part calculates a geoid height at each of the estimated positions based on the information about the geoid height.

Assignees

Inventors

Classifications

  • Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels (G01C3/20, G01C3/30 take precedence) · CPC title

  • specially adapted for use on moving platforms, e.g. ship, aircraft · CPC title

  • Determining velocity · CPC title

  • specially adapted for specific applications · CPC title

  • Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00 · 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 US11378397B2 cover?
A change in geoid height is measured easily. A geoid measurement method of the present invention executes an inertial measurement data acquiring step, a comparison data acquiring step, a state variable estimating step, and a geoid calculating step. In the inertial measurement data acquiring step, data related to velocity, position, and attitude angle is acquired as inertially-derived data based…
Who is the assignee on this patent?
Japan Aviation Electronics Ind Ltd, Tokyo Inst Tech
What technology area does this patent fall under?
Primary CPC classification G01C21/165. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Jul 05 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 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).