The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 25, 2020

Filed:

Apr. 27, 2018
Applicant:

Atlantic Inertial Systems Limited, Plymouth, Devon, GB;

Inventors:

Nicholas Mark Faulkner, Plymouth, GB;

John Keith Sheard, Plymouth, GB;

Assignee:

ATLANTIC INERTIAL SYSTEMS LIMITED, Plymouth, Devon, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 21/18 (2006.01); G01C 25/00 (2006.01); F42B 15/01 (2006.01);
U.S. Cl.
CPC ...
G01C 21/18 (2013.01); F42B 15/01 (2013.01); G01C 25/005 (2013.01);
Abstract

An inertial measurement system comprising: a first, roll gyro with an axis oriented substantially parallel to the spin axis of the projectile; a second gyro and a third gyro with axes arranged with respect to the roll gyro; a controller, arranged to: compute a current projectile attitude from the outputs of the first, second and third gyros; operate a Kalman filter that receives a plurality of measurement inputs including at least roll angle, pitch angle and yaw angle and that outputs at least a roll angle error; initialise the Kalman filter with a roll angle error uncertainty representative of a substantially unknown roll angle; generate at least one pseudo-measurement from stored expected flight data; provide said pseudo-measurement(s) to the corresponding measurement input of the Kalman filter; and apply the roll angle error from the Kalman filter as a correction to the roll angle.


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