Abstract: A monitoring system for alerting operators of aircraft or other vehicles when they are approaching a geographical feature of interest, such as a runway, taxiway or other aircraft. The system includes a database having at least one geo-referenced chart, a processor, a positioning system configured to identify a number of aircraft or other vehicle operational parameters and transmit that data to the processor, and a display unit configured to display the present position of the aircraft on the geo-referenced chart. After receiving the operational parameters, the processor identifies a virtual containment zone centered about the aircraft or vehicle. The processor further monitors the position of the aircraft or other vehicle relative to any geographical features of interest and determines whether at least a portion of a geographical feature is located within the containment area. If such a condition is detected, a notification is generated and presented to the operator who may respond accordingly.
Type:
Grant
Filed:
September 23, 2008
Date of Patent:
February 19, 2013
Assignee:
Universal Avionics Systems Corp.
Inventors:
Joachim Laurenz Naimer, Frank Hummel, David Zeitouni, Patrick Krohn
Abstract: A display image for use in an aircraft is produced in response to receiving aircraft location, heading, altitude, and pitch data. The location and heading data are employed to access a topographical database and obtain terrain information for a region on the earth's surface ahead of the aircraft. A terrain image is produced from the terrain information and a non-linear pitch scale is superimposed over the terrain image. The non-linear pitch scale corresponds to the relationship of the aircraft pitch and the terrain image. Additional data designating other aircraft operational parameters, such as speed and altitude, are depicted by graphical objects. The terrain image, the non-linear pitch scale, and the graphical objects are combined into the display image. The terrain image and the non-linear pitch scale move in the display image in response to changes in the pitch of the aircraft.
Type:
Grant
Filed:
November 14, 2007
Date of Patent:
November 2, 2010
Assignee:
Universal Avionics Systems Corp.
Inventors:
Joachim Laurenz Naimer, James Mitchell Brannen, John Russell Jorgensen, Cheng Wang, Patrick Krohn