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. 08, 2015

Filed:

Jun. 21, 2011
Applicant:

Robert D. Frey, Jr., Bolton, MA (US);

Inventor:

Robert D. Frey, Jr., Bolton, MA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G01S 19/53 (2010.01); G01S 19/18 (2010.01); G01S 5/02 (2010.01); F41G 7/34 (2006.01);
U.S. Cl.
CPC ...
G01S 19/18 (2013.01); F41G 7/346 (2013.01); G01S 5/0247 (2013.01); G01S 19/53 (2013.01);
Abstract

Disclosed is a system for determination of attitude for a projectile in flight. The system includes at least one antenna mounted on the projectile. Each antenna is configured to receive Global Positioning System (GPS) signals. Further, the system includes a signal receiving unit communicably coupled to the each antenna to receive the GPS signals and to ascertain the earth referenced velocity vector. The system also includes a plurality of magnetometers for ascertaining a projectile referenced earth's magnetic field vector. Moreover, the system includes a processing unit. The processing unit is configured to utilize a known projectile referenced velocity vector and a stored prediction of the earth referenced earth's magnetic field vector along with the measured earth referenced velocity vector and the measured projectile referenced earth's magnetic field vector to determine the attitude of the projectile. Further disclosed is a method for determination of attitude for a projectile in flight.


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