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. 12, 2015

Filed:

Sep. 19, 2012
Applicant:

Astrium Sas, Suresnes, FR;

Inventor:

Bernard Polle, Saint-Orens, FR;

Assignee:

Airbus Defence and Space SAS, Les Mureaux, FR;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/10 (2006.01); B64G 1/28 (2006.01); B64G 1/26 (2006.01); B64G 1/40 (2006.01); B64G 1/24 (2006.01); B64G 1/44 (2006.01);
U.S. Cl.
CPC ...
B64G 1/28 (2013.01); B64G 1/26 (2013.01); B64G 1/283 (2013.01); B64G 1/407 (2013.01); B64G 1/242 (2013.01); B64G 1/443 (2013.01); B64G 2001/245 (2013.01);
Abstract

A method of controlling the attitude of a satellite in orbit around a celestial body. The attitude of the satellite being controlled by a momentum storage device and controllable surfaces of the satellite configured to create desaturation torques in the storage device by using solar pressure. The controllable surfaces are arranged on solar panels mobile in rotation around an axis Y. At least one electric thruster configured to control the orbit of the satellite also controls the attitude of the satellite. The orientation of the electric thruster is controlled to activate the electric thruster with a thrust direction deliberately not aligned with a center of mass of the satellite to create desaturation torques in the storage device along axis Y. The controllable surfaces are controlled to create desaturation torques of the storage device in a plane orthogonal to the Y axis.


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