Patents by Inventor Rajanikanth Nagaraj Kashi

Rajanikanth Nagaraj Kashi has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 10037702
    Abstract: Methods and apparatus are provided for simulating an interval management (IM) procedure for an ownship aircraft and a target aircraft before the start of the performance of the IM procedure. The method comprises receiving an IM clearance message from air traffic control (ATC), parsing the received IM clearance message into parsed information components identifying the complexity of the IM clearance message based on the number of elements in the information components, generating a flight chart depicting the area over which the proposed IM procedure is to traverse using the mapping information wherein the flight chart includes a vertical view and a plan view, and simulating the IM procedure on the generated flight chart before any steps of the IM procedure are performed.
    Type: Grant
    Filed: July 19, 2017
    Date of Patent: July 31, 2018
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Rajanikanth Nagaraj Kashi, Vinayak Manohar Chitragar, Sathish Pakki
  • Patent number: 9704405
    Abstract: A method for generating a flight display in an aircraft includes the steps of receiving an indication of an arrival or a departure procedure for the aircraft to follow, receiving an indication of a current position and altitude of the aircraft, and receiving a voice communication or information by digital data link regarding the arrival or departure procedure. The method further includes the steps of recognizing speech in the voice communication and transforming the speech to a restriction regarding the arrival or departure procedure and providing a flight display comprising a visual depiction of the arrival or departure procedure, the current position and altitude of the aircraft, and the restriction regarding the arrival or departure procedure.
    Type: Grant
    Filed: June 12, 2014
    Date of Patent: July 11, 2017
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Rajanikanth Nagaraj Kashi, Divakara Rao Vadada, Cercuncesao Fernandes
  • Patent number: 9297895
    Abstract: 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.
    Type: Grant
    Filed: August 30, 2012
    Date of Patent: March 29, 2016
    Assignee: Honeywell International Inc.
    Inventors: Rajanikanth Nagaraj Kashi, Roger Rathbun, Scott Richard Gremmert, Dilip Mathews, Nainatara Kumble
  • Publication number: 20150364044
    Abstract: A method for generating a flight display in an aircraft includes the steps of receiving an indication of an arrival or a departure procedure for the aircraft to follow, receiving an indication of a current position and altitude of the aircraft, and receiving a voice communication or information by digital data link regarding the arrival or departure procedure. The method further includes the steps of recognizing speech in the voice communication and transforming the speech to a restriction regarding the arrival or departure procedure and providing a flight display comprising a visual depiction of the arrival or departure procedure, the current position and altitude of the aircraft, and the restriction regarding the arrival or departure procedure.
    Type: Application
    Filed: June 12, 2014
    Publication date: December 17, 2015
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Rajanikanth Nagaraj Kashi, Divakara Rao Vadada, Cercuncesao Fernandes
  • Publication number: 20150348421
    Abstract: 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.
    Type: Application
    Filed: August 30, 2012
    Publication date: December 3, 2015
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Rajanikanth Nagaraj Kashi, Roger Rathbun, Scott Richard Gremmert, Dilip Mathews, Nainatara Kumble
  • Patent number: 8818579
    Abstract: 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.
    Type: Grant
    Filed: August 30, 2012
    Date of Patent: August 26, 2014
    Assignee: Honeywell International Inc.
    Inventors: Rajanikanth Nagaraj Kashi, Roger Rathbun, Scott Richard Gremmert, Dilip Mathews, Nainatara Kumble
  • Publication number: 20140067171
    Abstract: 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.
    Type: Application
    Filed: August 30, 2012
    Publication date: March 6, 2014
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Rajanikanth Nagaraj Kashi, Roger Rathbun, Scott Richard Gremmert, Dilip Mathews, Nainatara Kumble