Honeywell International Inc.

Dilip Mathews

Scott Richard Gremmert

Rajanikanth Nagaraj Kashi

Nainatara Kumble

Roger Rathbun

Divya Swarup Giriyappa Srinivasan

David B Goldstein

Karthik Rao

Satish Kumar Rajendran

A method for updating aircraft data is provided. The method comprises: receiving one or more messages at a ground system that one or more aircraft is in a safe state on the ground; selecting one or more aircraft in the safe state to receive a software or database update from the ground system; verifying that the selected one or more aircraft in the safe state is in need of the software or database update; initiating a remote loading of the software or database update to the verified selected one or more aircraft in the safe state; and receiving one or more messages at the ground system from the verified selected one or more aircraft indicating a status of the remote loading.

Systems and methods for updating aircraft data based on location of aircraft

Systems and methods are operable to identify and indicate opportunities for an In-Trail procedure (ITP) aircraft to make an ITP altitude change. An exemplary embodiment receives information corresponding to a desired ITP altitude for the ITP aircraft and a projected window period; estimates at least one ITP maneuver opportunity window based on the estimated location of each of the plurality of other aircraft and based on a current airspeed and a current altitude of the ITP aircraft; generates a screen shot that presents an ITP maneuver opportunity window icon, wherein the ITP maneuver opportunity window icon graphically indicates the soonest time and the latest time that the ITP aircraft may initiate the ITP maneuver, and wherein the ITP maneuver opportunity window icon indicates an altitude change made by the ITP aircraft will maintain minimum safe self-separation distances from the plurality of other aircraft during the ITP maneuver.

Systems and methods for in-trail opportunity window estimator

Systems and methods are operable to present graphical information indicating capability of an aircraft to change altitude. An exemplary embodiment determines an altitude change capability of the aircraft; determines an altitude change capability icon based on the determined altitude change capability of the aircraft, wherein the altitude change capability icon is defined by at least a leading portion, a trailing portion, a top portion, and a bottom portion, wherein a slope of the leading portion of the altitude change capability icon corresponds to the determined altitude change capability of the aircraft, and wherein the leading portion and the trailing portion are separated by at least the top portion and the bottom portion; and communicates the altitude change capability icon to a display for presentation to the crew of the aircraft.

Systems and methods for graphically indicating aircraft ascent and descent capabilities

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Bengaluru, India

Dilip Mathews