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:
Jan. 07, 2020

Filed:

Jul. 25, 2017
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Brian O'Laughlin, Humboldt, AZ (US);

Mike Jackson, Maple Grove, MN (US);

Rajesh Chaubey, Karnataka, IN;

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); G08G 5/00 (2006.01); B64D 37/00 (2006.01); G01C 23/00 (2006.01); G06F 3/0488 (2013.01);
U.S. Cl.
CPC ...
G05D 1/0005 (2013.01); B64D 37/005 (2013.01); G08G 5/0021 (2013.01); G08G 5/0039 (2013.01); G08G 5/0052 (2013.01); G01C 23/00 (2013.01); G06F 3/0488 (2013.01);
Abstract

A method for computing a required speed profile for an aircraft to meet a required time of arrival (RTA) for a waypoint of a current flight is provided. During flight, the method calculates a fuel-efficient speed profile for the aircraft to meet the RTA for the waypoint, by a processor of a computing device communicatively coupled to one or more avionics systems onboard the aircraft; activates the fuel-efficient speed profile to fly the aircraft to the waypoint, by the processor; determines a priority between fuel efficiency of the fuel-efficient speed profile and time reliability, by the processor; and when the priority is the time reliability, switches from the fuel-efficient speed profile to a guidance margin control strategy to fly the aircraft to the waypoint, wherein the guidance margin control strategy increases the time reliability by enabling the aircraft to satisfy constraints of the RTA.


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