Methods and Apparatus for Determining Angle of Arrival (AOA) in a Radar Warning Receiver
First Claim
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1. A method, comprising;
- receiving signals from an emitter on a plurality of antennas of a radar warning receiver system;
determining an angle of arrival of the received signals from the emitter from first and second ones of the plurality of antennas;
determining a range for the emitter from a strength of the signals from the first and second ones of the plurality of antennas;
receiving navigational information for a vehicle to which the radar warning receiving is attached;
combining, using a computer processor, the aircraft attitude information with the range and the angle of arrival to determine a position of the emitter in three dimensions;
using navigation data to stabilize the three-dimensional emitter position against aircraft position changes;
applying tracking to the successive three-dimensional emitter location estimates to generate at least one track of position for the emitter; and
using the at least one track when information from the radar warning receiver is not available.
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Abstract
Methods and apparatus for determining an angle of arrival in a radar warning system that uses tracking to provide a more accurate angle of arrival than conventional systems. In exemplary embodiments, angle of arrival and range are mapped from measured body angles to a 3D coordinate system where modern tracking techniques are applied to improve accuracy and stabilization of measurements, then mapped back into body angles for display.
14 Citations
17 Claims
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1. A method, comprising;
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receiving signals from an emitter on a plurality of antennas of a radar warning receiver system; determining an angle of arrival of the received signals from the emitter from first and second ones of the plurality of antennas; determining a range for the emitter from a strength of the signals from the first and second ones of the plurality of antennas; receiving navigational information for a vehicle to which the radar warning receiving is attached; combining, using a computer processor, the aircraft attitude information with the range and the angle of arrival to determine a position of the emitter in three dimensions; using navigation data to stabilize the three-dimensional emitter position against aircraft position changes; applying tracking to the successive three-dimensional emitter location estimates to generate at least one track of position for the emitter; and using the at least one track when information from the radar warning receiver is not available. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
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10. An article, comprising:
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a non-transitory storage medium containing stored instructions that enable a machine to; receive signals from an emitter on a plurality of antennas of a radar warning receiver system; determine an angle of arrival of the received signals from the emitter from first and second ones of the plurality of antennas; determine a range for the emitter from a strength of the signals from the first and second ones of the plurality of antennas; receive navigational information for a vehicle to which the radar warning receiving is attached; combine the aircraft attitude information with the range and the angle of arrival to determine a position of the emitter in three dimensions; use navigation data to stabilize the three-dimensional emitter position against aircraft position changes; apply tracking to the successive three-dimensional emitter location estimates to generate at least one track of position for the emitter; and use the at least one track when information from the radar warning receiver is not available. - View Dependent Claims (11, 12, 13, 14, 15, 16)
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17. A system, comprising:
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a plurality of antennas of a radar warning receiver system to receive signals from an emitter; a radar warning system including a memory and a processor configured to; determine an angle of arrival of the received signals from the emitter from first and second ones of the plurality of antennas; determine a range for the emitter from a strength of the signals from the first and second ones of the plurality of antennas; receive navigational information for a vehicle to which the radar warning receiving is attached; combine the aircraft attitude information with the range and the angle of arrival to determine a position of the emitter in three dimensions; use navigation data to stabilize the three-dimensional emitter position against aircraft position changes; apply tracking to the successive three-dimensional emitter location estimates to generate at least one track of position for the emitter; and use the at least one track when information from the radar warning receiver is not available.
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Specification