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:
Oct. 18, 2022

Filed:

May. 16, 2019
Applicant:

Rosemount Aerospace Inc., Burnsville, MN (US);

Inventors:

Wesley J. Schwartz, Bloomington, MN (US);

Brian Brent Naslund, Chanhassen, MN (US);

John D. Winter, Apple Valley, MN (US);

Joel Boelke, Eden Prairie, MN (US);

Assignee:

ROSEMOUNT AEROSPACE INC., Burnsville, MN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); G01L 13/00 (2006.01); G01P 13/02 (2006.01); G06F 17/14 (2006.01); G06N 3/02 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); G01L 13/00 (2013.01); G01P 13/025 (2013.01); G06F 17/142 (2013.01); G06N 3/02 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A aircraft health management system for identifying an anomalous signal from one or more air data systems (ADS) includes one or more of a frequency processor, configured to provide a spectral signal that is representative of a frequency content of the first ADS signal, a noise processor, configured to provide a noise signal that is representative of a noise level of the first ADS signal, and a rate processor, configured to provide a rate signal that is representative of a rate of change of the first ADS signal. The aircraft health management system also includes a comparator configured to provide a differential signal between the first ADS signal and the second ADS signal, and a prognostic processor configured to determine if the ADS signal is anomalous by comparing values representative of a flight condition signal, the differential signal, and the spectral, noise, and/or rate signals.


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