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:
Feb. 27, 2024

Filed:

Apr. 29, 2021
Applicant:

Honeywell International S.r.o., Chodov, CZ;

Inventors:

Zdenek Kana, Dubnany, CZ;

Radek Baranek, Litovel, CZ;

Jindrich Dunik, Plzen, CZ;

Jussi Raasakka, Brno, CZ;

Milos Sotak, Ko{hacek over (s)}ice-{hacek over (S)}aca, SK;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01S 19/47 (2010.01); G01S 19/45 (2010.01); G01S 19/54 (2010.01); G01C 21/16 (2006.01); G01C 21/20 (2006.01); G01S 19/41 (2010.01); G01S 19/53 (2010.01); G01S 19/40 (2010.01);
U.S. Cl.
CPC ...
G01S 19/47 (2013.01); G01S 19/45 (2013.01); G01S 19/54 (2013.01); G01C 21/165 (2013.01); G01C 21/20 (2013.01); G01S 19/40 (2013.01); G01S 19/41 (2013.01); G01S 19/53 (2013.01);
Abstract

Systems and methods for estimating attitude and heading are provided. The systems and methods utilize carrier phase single difference (CSD) measurements or carrier phase double difference (CDD) measurements and a validation test for CSD or CDD measurement residuals. The systems and methods include applying a wrapping function with limit of ±half of the GNSS carrier signal wavelength to CSD or CDD measurement residuals to generate refined CSD or CDD measurement residuals and validating the refined CSD or CDD measurement residuals variance to determine valid CSD or CDD measurements. By using the validated CSD and CDD measurements, the systems and methods enable low grade hybrid inertial navigation systems to estimate attitude and heading with integrity and without a magnetometer or the need for integer ambiguity resolution even during the static or steady phases of flight/operation.


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