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. 16, 2021

Filed:

Nov. 14, 2018
Applicant:

Gulfstream Aerospace Corporation, Savannah, GA (US);

Inventor:

Kevin Prosser, Savannah, GA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01P 5/16 (2006.01); B64D 43/02 (2006.01); B64D 31/00 (2006.01); G07C 5/02 (2006.01); G07C 5/08 (2006.01); G06F 30/20 (2020.01); G01W 1/00 (2006.01); G06N 5/04 (2006.01); G08G 5/00 (2006.01); G06F 111/10 (2020.01);
U.S. Cl.
CPC ...
B64D 43/02 (2013.01); B64D 31/00 (2013.01); G01P 5/16 (2013.01); G01W 1/00 (2013.01); G06F 30/20 (2020.01); G06N 5/046 (2013.01); G07C 5/02 (2013.01); G07C 5/08 (2013.01); G08G 5/0034 (2013.01); G08G 5/0039 (2013.01); G08G 5/0091 (2013.01); G01W 2001/003 (2013.01); G06F 2111/10 (2020.01);
Abstract

Systems, methods, aircraft, non-transitory media, and memories are provided. An avionics system for an aircraft includes a storage device and one or more data processors. The storage device stores instructions for converting between airspeed types and the one or more data processors is configured to execute the instructions to: generate a calibrated airspeed of the aircraft; convert the calibrated airspeed to an actual true airspeed of the aircraft; determine an initial approximate relationship between the calibrated airspeed and a computed true airspeed as a function of a pressure altitude of the aircraft; generate an adjusted approximate relationship based on the actual true airspeed and the initial approximate relationship at a chosen pressure altitude; and estimate a future airspeed of the aircraft based on the adjusted approximate relationship and a future altitude.


Find Patent Forward Citations

Loading…