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.:

US 6990396 B1

PDF
Full Text
Expired
Date of Patent:
Jan. 24, 2006

Filed:

Dec. 13, 2002
Applicants:

Hanching Grant Wang, Hacienda Heights, CA (US);

Richard A. Fowell, Rolling Hills Estates, CA (US);

Che-hang C. Ih, Rancho Palos Verdes, CA (US);

Inventors:

Hanching Grant Wang, Hacienda Heights, CA (US);

Richard A. Fowell, Rolling Hills Estates, CA (US);

Che-Hang C. Ih, Rancho Palos Verdes, CA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 7/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method and an apparatus for controlling the attitude and momentum of a spacecraft while deploying an appendage from the spacecraft. The method comprises the steps of predicting an environmental torque the spacecraft will be subjected to during deployment of the appendage, computing a magnitude and a direction of momentum to add to the spacecraft to at least partially oppose the predicted environmental torque, and storing the computed magnitude and direction of momentum in at least one of the momentum wheels before deploying the appendage.


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Wang, Hanching. (2006). Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector (U.S. Patent No. 6990396). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/6990396

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