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:
Dec. 27, 2022

Filed:

Jul. 09, 2019
Applicant:

Deutsches Zentrum Fuer Luft- Und Raumfahrt E.v., Cologne, DE;

Inventors:

Winfried Halle, Berlin, DE;

Thomas Terzibaschian, Berlin, DE;

Christian Raschke, Schulzendorf, DE;

Wolfgang Baerwald, Berlin, DE;

Xavier Amiques, Berlin, DE;

Andreas Kotz, Petershagen, DE;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/28 (2006.01); G05D 1/00 (2006.01); B64G 1/24 (2006.01); G06T 7/70 (2017.01); B64G 1/36 (2006.01);
U.S. Cl.
CPC ...
B64G 1/244 (2019.05); B64G 1/285 (2013.01); B64G 1/288 (2013.01); B64G 1/36 (2013.01); G05D 1/0066 (2013.01); G06T 7/70 (2017.01);
Abstract

An attitude control apparatus for a satellite includes: at least three electric motors, wherein the at least three electric motors are arranged in such a way that a torque may be generated with any orientation of an associated torque vector, and a controller, wherein the controller is configured to drive the at least three electric motors based on a torque controller. The torque controller is adapted to operate the at least three electric motors outside a rest state only when an acceleration torque and a braking torque are required to execute an agile attitude change maneuver. There is also described an associated method.


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