Method and apparatus for estimation of center of gravity using accelerometers

US9568320B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9568320-B2
Application numberUS-201514704650-A
CountryUS
Kind codeB2
Filing dateMay 5, 2015
Priority dateMay 5, 2015
Publication dateFeb 14, 2017
Grant dateFeb 14, 2017

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

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A system and associated methodology determine navigation parameters of a vehicle under varying center of gravity position and varying unknown gravitational forces. The system uses high precision accelerometers arranged in a plurality of configurations.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for determining navigation parameters of a vehicle, the method comprising: receiving measurements from accelerometers; calculating, using processing circuitry, differential accelerometers measurements as a function of the measurements from the accelerometers; calculating, using the processing circuitry, an angular acceleration as a function of the differential accelerometers measurements under varying center of gravity position and unknown varying gravitational force with anomaly; calculating, using the processing circuitry, the square of the magnitude of an angular velocity as a function of the differential accelerometers measurements; and calculating, using the processing circuitry, the navigation parameters by determining the angular velocity using a Kalman filter as a function of the angular acceleration and the square of the magnitude of the angular velocity, wherein the calculation of the navigation parameters is fully operated in a passive navigation system. 2. The method of claim 1 , wherein the navigation parameters includes an inertial position, a velocity, an acceleration, an angular velocity, an angular acceleration, attitude, a position of a center of gravity and its rate of change, gravity tensor, and a gravitational acceleration. 3. The method of claim 2 , wherein the angular velocity estimation is isolated from gravity tensor estimation via a constrained filtering technique. 4. The method of claim 2 , wherein calculating the gravity tensor includes applying: Γ xx = - ( A 1 ⁢ x - A 2 ⁢ x ) 2 ⁢ µ - Ω z 2 - Ω y 2 Γ yy = - ( A 3 ⁢ y - A 4 ⁢ y ) 2 ⁢ µ - Ω z 2 - Ω x 2 Γ zz = - ( A 5 ⁢ z - A 6 ⁢ z ) 2 ⁢ µ - Ω x 2 - Ω y 2 Γ xy = - ( A 3 ⁢ x - A 4 ⁢ x ) + ( A 1 ⁢ y - A 2 ⁢ y ) 4 ⁢ µ + Ω x ⁢ Ω y Γ xz = - (

Assignees

Inventors

Classifications

  • G01M1/127Primary

    during the flight · CPC title

  • for gravity · CPC title

  • G01C21/16Primary

    by integrating acceleration or speed, i.e. inertial navigation · CPC title

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What does patent US9568320B2 cover?
A system and associated methodology determine navigation parameters of a vehicle under varying center of gravity position and varying unknown gravitational forces. The system uses high precision accelerometers arranged in a plurality of configurations.
Who is the assignee on this patent?
Univ King Fahd Pet & Minerals
What technology area does this patent fall under?
Primary CPC classification G01M1/127. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Feb 14 2017 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 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).