초록 ▼

An apparatus, method and computer program product for correcting own aircraft heading and displaying proximate aircraft traffic data on a Traffic Information Service display. The apparatus, method and computer program minimize slewing of the other aircraft data across the display during aircraft man

An apparatus, method and computer program product for correcting own aircraft heading and displaying proximate aircraft traffic data on a Traffic Information Service display. The apparatus, method and computer program minimize slewing of the other aircraft data across the display during aircraft maneuvers and provides a more reliable and consistent depiction of traffic relative to own aircraft position.

대표청구항 ▼

1. A method for showing on a display, the position of intruder aircraft relative to an own aircraft comprising the steps of: receiving a message uplinked from a ground station wherein said message includes a bearing of the intruder aircraft referenced from an uplinked groundtrack of the own aircr

1. A method for showing on a display, the position of intruder aircraft relative to an own aircraft comprising the steps of: receiving a message uplinked from a ground station wherein said message includes a bearing of the intruder aircraft referenced from an uplinked groundtrack of the own aircraft; comparing said uplinked groundtrack received in said message with a groundtrack measurement received from an airborne device; determining a correction by obtaining a difference between said uplinked groundtrack and said groundtrack measurement; applying said correction to said bearing to obtain a corrected bearing; and displaying the intruder aircraft on the display at said corrected bearing from the own aircraft. 2. A computer program product for displaying on a display the position of intruder aircraft relative to an own aircraft comprising: a computer readable storage medium having a computer readable program code means embedded in said medium, said computer readable program code means comprising: a first computer instruction means for receiving a message uplinked from a ground station wherein said message includes a bearing of the intruder aircraft referenced from an uplink groundtrack of the own aircraft; a second computer instruction means for comparing said uplinked groundtrack received in said message with a groundtrack measurement received from an airborne device; a third computer instruction means for determining a correction by obtaining a difference between said uplinked groundtrack and said groundtrack measurement; a fourth computer instruction means for applying said correction to said bearing to obtain a corrected bearing; and a fifth computer instruction means for displaying the intruder aircraft on the display at said corrected bearing from the own aircraft. 3. An apparatus for displaying intruder aircraft relative to an own aircraft in a Traffic Information System (TIS) comprising: an input coupled to receive: an uplinked message including a bearing of the intruder aircraft referenced from an uplinked groundtrack of the own aircraft; and a groundtrack measurement of the own aircraft received from an airborne sensor; an output; a signal processor, coupled to said input and to said output for: obtaining a difference between said uplinked groundtrack and said groundtrack measurement to obtain a bearing correction; and applying said bearing correction to said bearing to obtain a corrected bearing; outputting a signal useful for controlling a display to control display of the intruder aircraft relative to the own aircraft at said corrected bearing from the own aircraft. 4. An improvement to a Traffic Information Service (TIS) system, the improvement comprising: an airborne component for: (a) receiving an uplinked message including at least a bearing data of an intruder aircraft and an own aircraft groundtrack and for receiving an own aircraft groundtrack measurement from an airborne sensor; and (b) comparing said own aircraft groundtrack and said groundtrack measurement to obtain a correction to said bearing data. 5. The improvement of claim 4 further comprising a cockpit display coupled to said airborne component, wherein said cockpit displays a position of the intruder aircraft relative to the own aircraft using said correction to said bearing data.