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:
May. 24, 2022

Filed:

May. 29, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Cecilia G. Cantu, Playa Del Rey, CA (US);

Gary E. Lemke, Torrance, CA (US);

John Preston Charles Mills, Redondo Beach, CA (US);

Christopher James Wasson, Torrance, CA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/52 (2006.01); B64G 1/24 (2006.01); B64G 1/28 (2006.01); B64G 1/44 (2006.01); B64G 1/36 (2006.01);
U.S. Cl.
CPC ...
B64G 1/52 (2013.01); B64G 1/242 (2013.01); B64G 1/244 (2019.05); B64G 1/283 (2013.01); B64G 1/361 (2013.01); B64G 1/443 (2013.01); B64G 2001/245 (2013.01);
Abstract

A control system configured to execute a safing mode sequence for a spacecraft is disclosed. The control system includes one or more star trackers that each include a field of view to capture light from a plurality of space objects surrounding the celestial body. The control system also includes one or more actuators, one or more processors in electronic communication with the one or more actuators, and a memory coupled to the one or more processors. The memory stores data into a database and program code that, when executed by the one or more processors, causes the control system to determine a current attitude of the spacecraft, and re-orient the spacecraft from a current attitude into a momentum neutral attitude.


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