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:
Jul. 18, 2017

Filed:

Jun. 08, 2015
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Petr Vesely, Horni Marsov, CZ;

Petr Krupansky, Veverska Bityska, CZ;

Pavel Klang, Brno, CZ;

Jaroslav Jonak, Brno, CZ;

Michal Polansky, Brno, CZ;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G08G 5/02 (2006.01); G08G 5/04 (2006.01); G08G 5/00 (2006.01); G01S 13/93 (2006.01); G01S 13/91 (2006.01); G05D 1/10 (2006.01); G05D 1/06 (2006.01); G01C 23/00 (2006.01);
U.S. Cl.
CPC ...
G08G 5/02 (2013.01); G01C 23/005 (2013.01); G01S 13/9303 (2013.01); G05D 1/0676 (2013.01); G05D 1/104 (2013.01); G08G 5/0008 (2013.01); G08G 5/0021 (2013.01); G08G 5/0039 (2013.01); G08G 5/045 (2013.01); G01S 13/913 (2013.01); G08G 5/0052 (2013.01); G08G 5/025 (2013.01);
Abstract

This disclosure is directed to systems and methods for smart transitioning between aircraft trajectory management modes. In one example, a system is configured to track a speed of a target aircraft in flight ahead of an own aircraft on which the system is positioned. The system is further configured to determine whether the target aircraft has maintained a rate of change in speed within a selected range of variation in change of speed, for a selected period of time. The system is further configured to enable an activation of a merging trajectory management mode of the own aircraft in response to determining that the own aircraft is in a trajectory management mode transition airspace and that the target aircraft has maintained the rate of change in speed within the selected range of variation in change of speed, for the selected period of time.


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