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:
Oct. 10, 2023

Filed:

Mar. 04, 2021
Applicant:

Honeywell International Inc., Charlotte, NC (US);

Inventors:

Sally Ann Keyes, Minneapolis, MN (US);

Calvin Samborski, Saint Louis Park, MN (US);

Dean Richard Wilkens, Scottsdale, AZ (US);

Dale F. Enns, Roseville, MN (US);

Assignee:

Honeywell International Inc., Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F41G 7/36 (2006.01); F41G 7/00 (2006.01); F41G 7/22 (2006.01); F41G 7/34 (2006.01); F42B 15/01 (2006.01); G05D 1/10 (2006.01);
U.S. Cl.
CPC ...
F41G 7/36 (2013.01); F41G 7/007 (2013.01); F41G 7/222 (2013.01); F41G 7/2213 (2013.01); F41G 7/346 (2013.01); F42B 15/01 (2013.01); G05D 1/108 (2013.01);
Abstract

Model based inertial navigation for a spinning projectile is provided. In one embodiment, a navigation system comprises: a strapdown navigation processor; a propagator-estimator filter, the processor inputs inertial sensor data and navigation corrections from the filter to generate a navigation solution comprising projectile velocity and attitude estimates; an upfinding navigation aid that generates an angular attitude measurement indicative of a roll angle; and a physics model performing calculations utilizing dynamics equations for a rigid body, the model inputs 1) projectile state estimates from the navigation solution and 2) platform inputs indicative of forces acting on a projectile platform, and outputs a set of three orthogonal predicted translational acceleration measurements based on the inputs; the filter comprises a measurement equation associated with the physics model and the upfinding navigation aid and calculates the navigation corrections as a function of the navigation solution, the predicted translational acceleration measurements, and attitude measurement.


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