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:
Nov. 09, 2021

Filed:

Feb. 08, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Rongsheng Li, Hacienda Heights, CA (US);

Tung-Ching Tsao, Torrance, CA (US);

Harold A. Klotz, Jr., East Carondelet, IL (US);

Bruce M. Pope, Yorba Linda, CA (US);

Paul J. Haug, Saint Charles, MO (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01C 21/02 (2006.01); G01C 21/16 (2006.01); G05D 1/10 (2006.01); G06F 16/29 (2019.01);
U.S. Cl.
CPC ...
G01C 21/025 (2013.01); G01C 21/165 (2013.01); G05D 1/101 (2013.01); G06F 16/29 (2019.01);
Abstract

A celestial navigation system and method for determining a position of a vehicle. The system includes a star-tracker, a beam director, an inertial measurement unit, and a control module. The star-tracker has a field of view for capturing light. The beam director is configured to change a direction of the light captured in the field of view of the star-tracker. The inertial measurement unit has a plurality of sensors for measuring an acceleration and a rotation rate of the vehicle. The control module executes instructions to correct the attitude, the velocity and the position of the vehicle using the determined magnitude and position of the space objects. The control module also executes instructions to generate corrections to the IMU error parameters, the beam director and star-tracker alignment errors, and RSO ephemeris errors to achieve optimal performance.


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