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:

Feb. 01, 2012
Applicants:

Matthew W. Smith, Pasadena, CA (US);

Christopher M. Pong, Kaneohe, HI (US);

Sungyung Lim, Acton, MA (US);

David W. Miller, Sharon, MA (US);

Sara Seager, Concord, MA (US);

Shawn Murphy, Cambridge, MA (US);

Inventors:

Matthew W. Smith, Pasadena, CA (US);

Christopher M. Pong, Kaneohe, HI (US);

Sungyung Lim, Acton, MA (US);

David W. Miller, Sharon, MA (US);

Sara Seager, Concord, MA (US);

Shawn Murphy, Cambridge, MA (US);

Assignees:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 21/02 (2006.01); G05D 1/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

An optical system for use in an Earth-orbiting satellite includes a plurality of image sensors disposed on a focal plane having a reference axis orthogonal thereto, optics configured to focus incident light onto the image sensors, a piezoelectric actuator coupled to the image sensors and configured to translate the image sensors in at least two axes each orthogonal to the reference axis, and at least one controller operably coupled to the plurality of image sensors and the piezoelectric actuator. The image sensors are configured to generate at least one image frame from light detected by the plurality of image sensors, the image frame including a target star and at least one guide star. The controller is configured to stabilize the position of the target star by adjusting the position of the piezoelectric actuator based on the changes in the position of the guide star.


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