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 9038958 B1

PDF
Full Text
Expired
Date of Patent:
May. 26, 2015

Filed:

May. 23, 2013
Applicants:

Isaac Michael Ross, Monterey, CA (US);

Donghun Lee, Monterey, CA (US);

Mark Karpenko, Marina, CA (US);

Inventors:

Isaac Michael Ross, Monterey, CA (US);

Donghun Lee, Monterey, CA (US);

Mark Karpenko, Marina, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/28 (2006.01);
U.S. Cl.
CPC ...
B64G 1/286 (2013.01);
Abstract

Methods and apparatus are presented for spacecraft operation using non-Eigen axis attitude transitions via control momentum gyroscopes (CMGs) to avoid or mitigate singularities by providing a time-varying attitude command vector including a plurality of time-varying attitude command signals or values representing a plurality of spacecraft states and control trajectories as a guidance command input to an attitude controller of the spacecraft without modifying the spacecraft feedback control law.


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