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:
Aug. 25, 2020

Filed:

Mar. 09, 2018
Applicant:

Princeton Satellite Systems, Inc., Plainsboro, NJ (US);

Inventors:

Stephanie Thomas, West Windsor, NJ (US);

Michael A. Paluszek, Princeton, NJ (US);

Assignee:

PRINCETON SATELLITE SYSTEMS, INC., Plainsboro, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/36 (2006.01); G01L 3/00 (2006.01); G01R 33/02 (2006.01); G01R 33/07 (2006.01); H01F 5/00 (2006.01); B64G 1/32 (2006.01); H03H 17/02 (2006.01); H01F 6/06 (2006.01); B64G 1/24 (2006.01);
U.S. Cl.
CPC ...
B64G 1/366 (2013.01); B64G 1/32 (2013.01); G01L 3/00 (2013.01); G01R 33/0206 (2013.01); G01R 33/072 (2013.01); H01F 5/00 (2013.01); B64G 1/361 (2013.01); B64G 1/363 (2013.01); B64G 2001/245 (2013.01); B64G 2700/24 (2013.01); H01F 6/06 (2013.01); H03H 17/0257 (2013.01);
Abstract

A dipole cancellation system and method may include a plurality of magnetometers for measuring a device magnetic field associated with a plurality of device coils generating a device magnetic field having a primary magnetic dipole moment. A compensating coil carrying a compensating current running a first direction that generates a compensating magnetic field having a compensating magnetic dipole moment. The compensating coil may be positioned and the first current may be selected so that the compensating magnetic dipole moment completely cancels the primary magnetic dipole moment. A method may use the system to stabilize a spacecraft by calculating an estimated torque of the spacecraft, receiving a value for an external magnetic field, receiving a value for a device magnetic field, and calculating and applying a compensating current may be then applied to the compensating coil to cancel the primary magnetic dipole moment, wherein the spacecraft is stabilized.


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