Patents by Inventor Troy A. Nichols

Troy A. Nichols 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: 8219265
    Abstract: A display system and method for an aircraft simultaneously displays the terrain under the flight plan, or under the current track of the aircraft, as both a two-dimensional lateral situation view image and as a perspective vertical situation view image. This provides improved tactical flight planning, and that does not erroneously show the flight plan passing through the displayed terrain.
    Type: Grant
    Filed: August 25, 2009
    Date of Patent: July 10, 2012
    Assignee: Honeywell International Inc.
    Inventors: David B. Dwyer, Troy A. Nichols, Mathew Hilbert, Michael C. Little
  • Patent number: 8095249
    Abstract: Methods and systems for displaying a digital terrain to a user of a vehicle are provided. First, second, and third actual terrain data points are received. The third actual terrain data point is between the first and second actual terrain data points. If the third actual terrain data point is above a line interconnecting the first and second actual terrain data points, the first actual terrain data point is modified such that the third actual terrain data point is not above a line interconnecting said modified first actual terrain data point and the second actual terrain data point. A digital terrain is displayed to the user of the vehicle. The digital terrain includes a first digital terrain data point corresponding to the modified first actual terrain data point.
    Type: Grant
    Filed: September 4, 2007
    Date of Patent: January 10, 2012
    Assignee: Honeywell International Inc.
    Inventors: Michael C. Little, Troy A. Nichols
  • Publication number: 20100070109
    Abstract: Methods and systems for displaying a digital terrain to a user of a vehicle are provided. First, second, and third actual terrain data points are received. The third actual terrain data point is between the first and second actual terrain data points. If the third actual terrain data point is above a line interconnecting the first and second actual terrain data points, the first actual terrain data point is modified such that the third actual terrain data point is not above a line interconnecting said modified first actual terrain data point and the second actual terrain data point. A digital terrain is displayed to the user of the vehicle. The digital terrain includes a first digital terrain data point corresponding to the modified first actual terrain data point.
    Type: Application
    Filed: September 4, 2007
    Publication date: March 18, 2010
    Applicant: HONEYWELL INTERNATIONAL, INC.
    Inventors: Michael C. Little, Troy A. Nichols
  • Publication number: 20090319103
    Abstract: A display system and method for an aircraft simultaneously displays the terrain under the flight plan, or under the current track of the aircraft, as both a two-dimensional lateral situation view image and as a perspective vertical situation view image. This provides improved tactical flight planning, and that does not erroneously show the flight plan passing through the displayed terrain.
    Type: Application
    Filed: August 25, 2009
    Publication date: December 24, 2009
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: David B. Dwyer, Troy A. Nichols, Mathew Hilbert, Michael C. Little
  • Publication number: 20090312893
    Abstract: A display system and method for an aircraft simultaneously displays the terrain under the flight plan, or under the current track of the aircraft, as both a two-dimensional lateral situation view image and as a perspective vertical situation view image. This provides improved tactical flight planning, and that does not erroneously show the flight plan passing through the displayed terrain.
    Type: Application
    Filed: August 25, 2009
    Publication date: December 17, 2009
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: David B. Dwyer, Troy A. Nichols, Mathew Hilbert, Michael C. Little
  • Patent number: 7603209
    Abstract: A display system and method for an aircraft simultaneously displays the terrain under the flight plan, or under the current track of the aircraft, as both a two-dimensional lateral situation view image and as a perspective vertical situation view image. This provides improved tactical flight planning, and that does not erroneously show the flight plan passing through the displayed terrain.
    Type: Grant
    Filed: May 27, 2004
    Date of Patent: October 13, 2009
    Assignee: Honeywell International Inc.
    Inventors: David B. Dwyer, Troy A. Nichols, Matthew Hilbert, Michael C. Little
  • Patent number: 7295901
    Abstract: An avionics system includes a display device that is viewable by a user of an aircraft and a processor in operable communication with the display device. The processor is configured to display a digital terrain having a digital landmark thereon on the display device, the digital terrain being representative of an actual terrain and the digital landmark being representative of an actual landmark on the actual terrain, and display a plurality of position indicators over the digital terrain such that a line extending through the plurality of position indicators intersects the digital landmark, the position indicators being a fixed digital terrain distance apart as measured over the digital terrain.
    Type: Grant
    Filed: September 25, 2006
    Date of Patent: November 13, 2007
    Assignee: Honeywell International, Inc.
    Inventors: Michael C. Little, Troy A. Nichols
  • Patent number: 7209070
    Abstract: A vertical situation display (“VSD”) system according to the invention generates a terrain image that represents a profile view of terrain elevation relative to the position of an aircraft traveling above the terrain. The VSD system generates the VSD image such that the terrain image is biased toward the lower elevation region of the VSD screen, thus making efficient use of the available display area. The VSD image is also generated such that it is continuous across the lateral range of the VSD, thus ensuring that terrain is shown in the VSD at all practical times, depending upon the available range and any priority display rules.
    Type: Grant
    Filed: October 7, 2004
    Date of Patent: April 24, 2007
    Assignee: Honeywell International, Inc.
    Inventors: William R. Gilliland, Troy A. Nichols