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:
Jun. 05, 2018

Filed:

Nov. 24, 2014
Applicant:

Airbus Defence and Space Sas, Toulouse, FR;

Inventors:

Nicolas Cuilleron, Toulouse, FR;

Jean Sperandei, Toulouse, FR;

Philippe Laurens, Beauteville, FR;

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/28 (2006.01); B64G 1/44 (2006.01); B64G 1/40 (2006.01); B64G 1/24 (2006.01);
U.S. Cl.
CPC ...
B64G 1/443 (2013.01); B64G 1/242 (2013.01); B64G 1/283 (2013.01); B64G 1/286 (2013.01); B64G 1/405 (2013.01);
Abstract

A method to control a sunlight acquisition phase of a spacecraft with a nonzero angular momentum of an axis D. The spacecraft includes a solar generator configured to rotate about an axis Y. The spacecraft actuators are controlled to place the spacecraft in an intermediate orientation in which the axis Y is substantially orthogonal to the axis D. The solar generator is controlled to orientate the solar generator towards the sun. The spacecraft actuators are controlled to reduce the angular momentum of the spacecraft. The actuators of the spacecraft engine are controlled to place the spacecraft in an acquisition orientation in which the axis Y is substantially orthogonal to the direction of the sun with respect to the spacecraft.


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