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:
Dec. 22, 2015

Filed:

Nov. 03, 2014
Applicants:

Mikhail S. Belenkii, San Diego, CA (US);

Timothy Brinkley, San Diego, CA (US);

Inventors:

Mikhail S. Belenkii, San Diego, CA (US);

Timothy Brinkley, San Diego, CA (US);

Assignee:

Trex Enterprises Corp., San Diego, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 21/10 (2006.01); G01C 21/02 (2006.01); G01C 21/18 (2006.01); G01S 19/40 (2010.01); G01C 21/16 (2006.01); G01S 19/47 (2010.01); G01S 5/16 (2006.01); B64G 1/36 (2006.01); G01C 15/00 (2006.01); B64G 1/24 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
G01C 21/025 (2013.01); G01C 21/165 (2013.01); G01C 21/18 (2013.01); G01S 19/40 (2013.01); G01S 19/47 (2013.01); B64G 1/24 (2013.01); B64G 1/36 (2013.01); G01C 15/00 (2013.01); G01C 15/002 (2013.01); G01C 21/10 (2013.01); G01S 5/16 (2013.01); G05D 1/0883 (2013.01);
Abstract

An angles only navigation system. The system includes an IMU coupled with a passive optical sensor. The optical sensor provides periodic updates to the IMU in order to correct for accelerometer and gyro drifts. The IMU computes the air vehicle's instantaneous position, velocity, and attitude using gyro and accelerometer measurements. The optical sensor images stars and satellites. The navigation filter combines optical sensor measurements with IMU inputs, and determines those corrections needed to compensate for the IMU drifts. By applying periodic corrections to the IMU using satellite angular measurements, the navigation filter maintains an accurate position estimate during an entire flight.


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