Method for determining conflicting paths between mobile airborne vehicles and associated system and computer software program product
First Claim
1. A method of determining conflicting flight paths between a first airborne vehicle and a second airborne vehicle, the vehicles being adapted to be airborne above the earth, the earth being shaped as an oblate spheroid having a curvature, said method comprising:
- determining a position and a velocity vector for each of the first airborne vehicle and the second airborne vehicle;
defining a cylindrical volume about the first airborne vehicle, the first airborne vehicle being centrally disposed therein;
determining a separation distance between the first airborne vehicle and the second airborne vehicle at a selected time, the separation distance being at least partially determined from the position and the velocity vector of each vehicle and being adjusted with respect to the curvature of the earth using a great circle earth model;
determining an accuracy factor for the position of each vehicle;
modifying the separation distance by the accuracy factor; and
determining whether the modified separation distance is within the cylindrical volume about the first airborne vehicle during a time range so as to determine whether conflicting flight paths exist between the first airborne vehicle and the second airborne vehicle.
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Accused Products
Abstract
A method of determining conflicting flight paths between a first and a second airborne vehicle is provided, wherein each vehicle comprises an aircraft-to-aircraft navigational communication system having a navigational device. First, a position and a velocity vector are determined for each of the airborne vehicles. A cylindrical volume is then defined about the first airborne vehicle. A separation distance is then determined between the vehicles at a selected time and using a great circle earth model. An accuracy factor is thereafter determined for the position of each vehicle. The separation distance is then modified by the accuracy factor. A determination is then made as to whether the modified separation distance is within the cylindrical volume about the first airborne vehicle during a time range to thereby determine whether conflicting flight paths exist between the vehicles. An associated system and computer software program product are also provided.
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Citations
58 Claims
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1. A method of determining conflicting flight paths between a first airborne vehicle and a second airborne vehicle, the vehicles being adapted to be airborne above the earth, the earth being shaped as an oblate spheroid having a curvature, said method comprising:
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determining a position and a velocity vector for each of the first airborne vehicle and the second airborne vehicle;
defining a cylindrical volume about the first airborne vehicle, the first airborne vehicle being centrally disposed therein;
determining a separation distance between the first airborne vehicle and the second airborne vehicle at a selected time, the separation distance being at least partially determined from the position and the velocity vector of each vehicle and being adjusted with respect to the curvature of the earth using a great circle earth model;
determining an accuracy factor for the position of each vehicle;
modifying the separation distance by the accuracy factor; and
determining whether the modified separation distance is within the cylindrical volume about the first airborne vehicle during a time range so as to determine whether conflicting flight paths exist between the first airborne vehicle and the second airborne vehicle. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
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20. A system for determining conflicting flight paths between a first airborne vehicle and a second airborne vehicle, the vehicles being adapted to be airborne above the earth, the earth being shaped as an oblate spheroid having a curvature, said system comprising:
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a computer device housed by the first airborne vehicle, the computer device comprising;
a processing portion for determining a position and a velocity vector for each of the first airborne vehicle and the second airborne vehicle;
a processing portion for defining a cylindrical volume about the first airborne vehicle, the first airborne vehicle being centrally disposed therein;
a processing portion for determining a separation distance between the first airborne vehicle and the second airborne vehicle at a selected time, the separation distance being at least partially determined from the position and the velocity vector of each vehicle and being adjusted with respect to the curvature of the earth using a great circle earth model;
a processing portion for determining an accuracy factor for the position of each vehicle, a processing portion for modifying the separation distance by the accuracy factor; and
a processing portion for determining whether the modified separation distance is within the cylindrical volume about the first airborne vehicle during a time range so as to determine whether conflicting flight paths exist between the first airborne vehicle and the second airborne vehicle. - View Dependent Claims (21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39)
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40. A computer software program product capable of being executed by a computer device so as to determine conflicting flight paths between a first airborne vehicle and a second airborne vehicle, the vehicles being adapted to be airborne above the earth, the earth being shaped as an oblate spheroid having a curvature, the computer software program product comprising:
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an executable portion capable of determining a position and a velocity vector for each of the first airborne vehicle and the second airborne vehicle;
an executable portion capable of defining a cylindrical volume about the first airborne vehicle such that the first airborne vehicle is centrally disposed therein;
an executable portion capable of determining a separation distance between the first airborne vehicle and the second airborne vehicle at a selected time, the separation distance being at least partially determined from the position and the velocity vector of each vehicle and being adjusted with respect to the curvature of the earth using a great circle earth model;
an executable portion capable of determining an accuracy factor for the position of each vehicle;
an executable portion capable of modifying the separation distance by the accuracy factor; and
an executable portion capable of determining whether the modified separation distance is within the cylindrical volume about the first airborne vehicle during a time range so as to determine whether conflicting flight paths exist between the first airborne vehicle and the second airborne vehicle. - View Dependent Claims (41, 42, 43, 44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58)
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Specification