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:
Jul. 08, 2014

Filed:

Nov. 16, 2010
Applicants:

Chan Gook Park, Seoul, KR;

Jun Han Lee, Seoul, KR;

Won Hee Lee, Seoul, KR;

Inventors:

Chan Gook Park, Seoul, KR;

Jun Han Lee, Seoul, KR;

Won Hee Lee, Seoul, KR;

Assignee:

SNU R&DB Foundation, Seoul, KR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01M 17/00 (2006.01); B64G 1/24 (2006.01); B64G 1/26 (2006.01); B64G 1/28 (2006.01);
U.S. Cl.
CPC ...
B64G 1/24 (2013.01); B64G 1/26 (2013.01); B64G 1/283 (2013.01);
Abstract

Provided are a fault detector and a fault detection method for an attitude control system (ACS) of a spacecraft. The fault detector includes a first interacting multiple model (IMM) fault detection block for generating a normal model filter of the plurality of actuators and a plurality of upper level filters including fault model filters corresponding to the respective actuators, and detecting faults of the plurality of actuators using an IMM estimation technique from the plurality of upper level filters, and a second IMM fault detection block for generating a plurality of lower level filters each including a fault type model filter of the fault-detected actuator in the first IMM fault detection block, and detecting a fault type of the failed actuator using the IMM estimation technique.


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