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:
Mar. 31, 2020

Filed:

Jun. 12, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Jia Luo, Bellevue, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01P 5/14 (2006.01); G06F 17/50 (2006.01); G01P 5/00 (2006.01); G01P 21/02 (2006.01); G01P 13/02 (2006.01);
U.S. Cl.
CPC ...
G01P 5/14 (2013.01); G01P 5/00 (2013.01); G01P 13/025 (2013.01); G01P 21/025 (2013.01); G06F 17/5009 (2013.01); G06F 2217/16 (2013.01);
Abstract

A system and method for estimating a plurality of airspeed parameters of an aircraft is disclosed. The system comprises one or more processors and a memory coupled to the processor. The memory storing data comprising a database and program code that, when executed by the one or more processors, causes the system to receive a plurality of operating parameters that each represent an operating condition of the aircraft. The system is further caused to determine a model based dynamic pressure based on the operating parameters. The model based dynamic pressure is estimated based on steady flight conditions of the aircraft. The system is further caused to determine a bridge based dynamic pressure based on at least a temperature deviation and an inertial speed vector. The bridge based dynamic pressure is estimated for extreme flight conditions of the aircraft.


Find Patent Forward Citations

Luo, Jia. (2020). System for estimating airspeed of an aircraft based on a weather buffer model (U.S. Patent No. 10605822). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10605822

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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