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. 14, 2016

Filed:

Oct. 25, 2013
Applicant:

Airbus Defence and Space Sas, Les Mureaux, FR;

Inventor:

Valerio Moro, Toulouse, FR;

Assignee:

AIRBUS DEFENCE AND SPACE SAS, Les Mureaux, FR;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/36 (2006.01); B64G 1/32 (2006.01); G05D 1/08 (2006.01); G01L 3/10 (2006.01); G01L 5/00 (2006.01); G01L 5/22 (2006.01); B64G 1/24 (2006.01);
U.S. Cl.
CPC ...
B64G 1/32 (2013.01); B64G 1/366 (2013.01); G01L 3/101 (2013.01); G01L 5/0042 (2013.01); G01L 5/22 (2013.01); G05D 1/0883 (2013.01); B64G 2001/245 (2013.01);
Abstract

A method of command of magneto-torquers of an attitude control system of a space vehicle subjected to an external magnetic field of variable direction. The magneto-torquers are configured to desaturate an angular momentum storage device by transferring angular momentum and configured to form, in cooperation with the local external magnetic field, magnetic couples in a plane orthogonal to the direction of the local external magnetic field or a local control plane. The magnetic couple to be formed in the local control plane is determined as a function of the component of a desired attitude control couple which is orthogonal to the local control plane or a locally uncontrollable component. The contribution of the locally uncontrollable component to the magnetic couple to be formed is non-zero when the locally uncontrollable component is non-zero.


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