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.
Patent No.:
Date of Patent:
Apr. 04, 2000
Filed:
Jun. 26, 1997
Applicant:
Inventors:
Yeong-Wei Andy Wu, Rancho Palos Verdes, CA (US);
Garry Didinsky, Los Angeles, CA (US);
Douglas H Hein, Los Angeles, CA (US);
Assignee:
Hughes Electronics Corporation, Los Angeles, CA (US);
Primary Examiner:
Int. Cl.
CPC ...
G06F / ; B64G / ;
U.S. Cl.
CPC ...
701 13 ; 701-8 ; 701-3 ; 244164 ; 244165 ; 244171 ; 250330 ; 73 10 ; 73-179 ;
Abstract
Spacecraft attitude is efficiently controlled by utilizing spatial noise and temporal noise in the calculation of gains to a Kalman filter. Spatial noise is modeled in a dynamic fashion so as to provide optimal spatial noise attenuation.
Quick Actions:
Wu, Yeong-Wei. (2000). Enhanced stellar attitude determination system (U.S. Patent No. 6047226). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/6047226
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