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. 20, 2016

Filed:

Aug. 27, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

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

Arunkumar Pursayya Nayak, Van Nuys, CA (US);

Kangsik Lee, Torrance, CA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/26 (2006.01); B64G 1/28 (2006.01); B64G 1/40 (2006.01); G05D 1/08 (2006.01); G07C 5/08 (2006.01); B64G 1/24 (2006.01);
U.S. Cl.
CPC ...
B64G 1/26 (2013.01); B64G 1/283 (2013.01); B64G 1/405 (2013.01); G05D 1/0883 (2013.01); G07C 5/0808 (2013.01); B64G 2001/245 (2013.01);
Abstract

Apparatus and methods for attitude control of a space vehicle. The space vehicle includes a reaction wheel subsystem and a propulsion subsystem for attitude control. A slew controller for the space vehicle detects a failure of the reaction wheel subsystem. To perform an attitude slew, the slew controller identifies a pair of thrusters in the propulsion subsystem that will rotate the space vehicle about a desired axis. The slew controller determines burn parameters for the pair of thrusters, and initiates the burns to perform the desired attitude slew.


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