Patents by Inventor John Thomas Anders

John Thomas Anders 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: 8485029
    Abstract: An aircraft 160 approaches a landing point 162 following a flight path 164 to a designation point 166, the pilot sights the landing point 162 and activates the apparatus. A first calculation of coordinates for the landing point 162 is made and landing symbology generated. The pilot reviews the landing symbology and decides whether or not there is an acceptable correlation with the landing point 162. If not, the pilot will continue along the flight path 164 activating the apparatus at further designation points 168, 170 and 172 to reduce the designation error between the coordinates calculated by the apparatus and the real world landing position 162 observed by the pilot until the pilot is satisfied. At this point the pilot enters a landing phase and the symbology provides the pilot with landing cues even when the helicopter 160 enters a brown out event indicated by cloud 174.
    Type: Grant
    Filed: September 23, 2011
    Date of Patent: July 16, 2013
    Assignee: BAE Systems PLC
    Inventor: John Thomas Anders
  • Patent number: 8286477
    Abstract: An aircraft 160 approaches a landing point 162 following a flight path 164 to a designation point 166, the pilot sights the landing point 162 and activates the apparatus. A first calculation of coordinates for the landing point 162 is made and landing symbology generated. The pilot reviews the landing symbology and decides whether or not there is an acceptable correlation with the landing point 162. If not, the pilot will continue along the flight path 164 activating the apparatus at further designation points 168, 170 and 172 to reduce the designation error between the coordinates calculated by the apparatus and the real world landing position 162 observed by the pilot until the pilot is satisfied. At this point the pilot enters a landing phase and the symbology provides the pilot with landing cues even when the helicopter 160 enters a brown out event indicated by cloud 174.
    Type: Grant
    Filed: November 14, 2008
    Date of Patent: October 16, 2012
    Assignee: Bae Systems PLC
    Inventor: John Thomas Anders
  • Publication number: 20120139759
    Abstract: An aircraft 160 approaches a landing point 162 following a flight path 164 to a designation point 166, the pilot sights the landing point 162 and activates the apparatus. A first calculation of coordinates for the landing point 162 is made and landing symbology generated. The pilot reviews the landing symbology and decides whether or not there is an acceptable correlation with the landing point 162. If not, the pilot will continue along the flight path 164 activating the apparatus at further designation points 168, 170 and 172 to reduce the designation error between the coordinates calculated by the apparatus and the real world landing position 162 observed by the pilot until the pilot is satisfied. At this point the pilot enters a landing phase and the symbology provides the pilot with landing cues even when the helicopter 160 enters a brown out event indicated by cloud 174.
    Type: Application
    Filed: September 23, 2011
    Publication date: June 7, 2012
    Applicant: BAE SYSTEMS plc
    Inventor: John Thomas ANDERS
  • Publication number: 20110254855
    Abstract: A helmet-mounted display system or a head-mounted display system comprises an imaging means for presenting to a user a first image of a real field of view, means for presenting a second image superimposed on the first image, and control means for controlling the contrast between the first and second images so as to maintain the visibility to the user of the second image.
    Type: Application
    Filed: December 17, 2009
    Publication date: October 20, 2011
    Applicant: BAE SYSTEMS plc
    Inventor: John Thomas Anders
  • Publication number: 20100156758
    Abstract: An aircraft (160) approaches a landing point (162) following a flight path (164) to a designation point (166), the pilot sights the landing point (162) and activates the apparatus. A first calculation of coordinates for the landing point (162) is made and landing symbology generated. The pilot reviews the landing symbology and decides whether or not there is an acceptable correlation with (10) the landing point (162). If not, the pilot will continue along the flight path (164) activating the apparatus at further designation points (168, 170 and 172) to reduce the designation error between the coordinates calculated by the apparatus and the real world landing position (162) observed by the pilot until the pilot is satisfied. At this point the pilot enters a landing phase and the (15) symbology provides the pilot with landing cues even when the helicopter (160) enters a brown out event indicated by cloud (174).
    Type: Application
    Filed: November 14, 2008
    Publication date: June 24, 2010
    Inventor: John Thomas Anders