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:
Sep. 16, 2025

Filed:

Jan. 26, 2021
Applicants:

Safran Electronics & Defense, Paris, FR;

M3 Systems, L'Union, FR;

Inventors:

Philippe Elie, Paris, FR;

Vincent Bisgambiglia, Paris, FR;

Elie Amani, L'Union, FR;

Marc Pollina, L'Union, FR;

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G01S 19/49 (2010.01); G01S 5/02 (2010.01); G01S 19/46 (2010.01); G01C 21/16 (2006.01); G01S 19/45 (2010.01); G01S 19/48 (2010.01);
U.S. Cl.
CPC ...
G01S 19/49 (2013.01); G01S 5/0264 (2020.05); G01S 19/46 (2013.01); G01C 21/165 (2013.01); G01S 19/45 (2013.01); G01S 19/48 (2013.01);
Abstract

Navigation device including an inertial navigation system coupled with a satellite navigation system, the information supplied by the satellite positioning system being used for adjusting the inertial navigation system, characterised in that the device further comprises means for measuring signals coming from base stations of a wireless cellular network, the satellite navigation system and the means for measuring signals coming from base stations of the wireless cellular network are coupled with each other by a tight coupling to form a satellite navigator and/or base-station navigator implementing an estimator with simultaneous localisation and mapping, and in that the satellite navigation system and the means for measuring signals coming from base stations of the wireless cellular network are coupled to the inertial navigation system by a loose coupling for adjusting the inertial navigation system.


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