System and method for resolving phase ambiguity of a transducer array to determine direction of arrival of received signals

• US 7,380,455 B2
• Filed: 01/09/2007
• Issued: 06/03/2008
• Est. Priority Date: 10/18/2004
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Workman, Wayne C.
• Primary Examiner(s): Williams; Hezron E.
• Assistant Examiner(s): MILLER, ROSE MARY
• Application Number:
  US11/621,529
• Publication Number:
  US 20070219742A1
• Time in Patent Office: 511 Days
• Field of Search: None
• US Class Current: 73/602
• CPC Class Codes: G01N 2291/106 one or more transducer arrays
• CPC Class Codes: G01N 29/0618 synchronised with scanning, e.g. in real-time
• CPC Class Codes: G01N 29/262 by electronic orientation or focusing, e.g. with phased arrays phased arrays per se G10K11/34

Abstract

System and method for resolving phase ambiguities of various transducer arrays, including non-coplanar interferometer antennas on an aircraft skin, in order to determine the direction of arrival of a signal received by the array and emitted by a source remote from the array.

Claims

1. A system for determining a direction of arrival of a signal emitted by a source and for resolving front to back phase ambiguity, said system comprising:

a plurality of at least four non-collinear, non-coplanar, spaced transducers, each receiving the emitted signal and providing a transducer output signal corresponding to the received emitted signal;

a multi-channel receiver, each channel associated with one of the transducers for receiving each associated transducer output signal and providing a receiver output signal indicating the phase of the received signal;

a processor for receiving the receiver output signals and for processing the received transducer output signals by employing a direction finding algorithm to minimize phase ambiguities between the receiver output signals to determine a first direction and a second direction, said processor for determining an amplitude comparison between two of the received transducer output signals of the transducer elements and of the received transducer output signal of another transducer element receiving from a direction substantially opposite to a direction in which of the two transducers receive, and said processor selecting the first direction or the second direction as a function of the determined amplitude comparison, said selected direction corresponding to the direction of arrival of the emitted signal relative to the transducers.

2. The system of claim 1 wherein the transducers are antennas mounted on a surface of an aircraft.

3. The system of claim 1 wherein the transducers are selected from the following:

antennas, rf sensors, sonaphones, sound sensors, seismic sensors, acoustic wave sensors and/or pressure sensors.

4. The system of claim 1 wherein:

a first channel of the receiver receives a first transducer output signal and provides a first channel output signal having a phase corresponding to the phase of the signal received by a first transducer of the plurality of transducers;

a second channel of the receiver receives the second transducer output signal and provides a second channel output signal having a phase corresponding to the phase of the signal received by a second transducer of the plurality of transducers; and

the processor receives the first channel output signal and the second channel output signal and provides an output signal corresponding to the direction of arrival.

5. The system of claim 4 wherein the plurality of transducers comprises a first transducer and a second transducer and further comprising:

a third transducer receiving the emitted signal and providing a third transducer output signal corresponding to the emitted signal received by a third transducer of the plurality of transducers, said third transducer spaced a distance D₂₃ from the second transducer;

a third channel of the receiver for receiving the third transducer output signal and providing a third channel output signal indicating the phase of the third transducer output signal received by the third transducer; and

said processor receives the third channel output signal, said processor determining a set of interferometer planes corresponding to a phase difference between the second transducer output signal and the third transducer output signal, said phase difference being a function of the distance D₂₃, and said processor providing output information corresponding to a direction of arrival of the emitted signal relative to the first, second and third transducers, wherein the output information is a function of an intersection of the set of interferometer planes with a direction cosine sphere.

6. The system of claim 5 wherein said processor determines said amplitude comparison as a function of a distance D₂₃ between the second transducer and the third transducer.

7. The system of claim 6 wherein the transducers are antennas mounted on a surface of an aircraft.

8. The system of claim 1 wherein said processor determines said amplitude comparison as a function of a distance between two of said plurality of transducers.

9. A method for determining a direction of arrival of a signal emitted by a source and for resolving front to back phase ambiguity, said method comprising:

receiving the emitted signal via a plurality of at least four non-collinear, non-coplanar, spaced transducers, and providing a transducer output signal corresponding to the received emitted signal from each transducer;

receiving each associated transducer output signal and providing a receiver output signal indicating the phase of the received emitted signal;

processing the received transducer output signals by employing a direction finding algorithm to minimize phase ambiguities between the received transducer output signals to determine a first direction and a second direction;

determining an amplitude comparison between the received transducer output signals of two of the transducer elements and the received transducer output signal of another transducer element receiving from a direction substantially opposite to a direction in which of the two transducers receive;

selecting the first direction or the second direction as a function of the determined amplitude comparison, said selected direction corresponding to the direction of arrival of the emitted signal relative to the transducers.

10. The method of claim 9 wherein the transducers are antennas mounted on a surface of an aircraft.

11. The method of claim 9 wherein the transducers are selected from the following:

antennas, rf sensors, sonaphones, sound sensors, seismic sensors, acoustic wave sensors and/or pressure sensors.

12. The method of claim 9 wherein receiving the emitted signal comprises receiving the emitted signal via a first transducer of the plurality of transducers and providing a first transducer output signal corresponding to the emitted signal received by the first transducer, and further comprising providing a first output signal having a phase corresponding to the phase of the received first transducer output signal;

wherein receiving the emitted signal comprises receiving the emitted signal via a second transducer of the plurality of transducers and providing a second transducer output signal corresponding to the emitted signal received by the second transducer, and further comprising;

providing a second output signal having a phase corresponding to the phase of the second transducer output signal;

receiving the first output signal and the second output signal; and

providing an output signal corresponding to the direction of arrival.

13. The method of claim 12 wherein receiving the emitted signal comprises receiving the emitted signal via a third transducer of the plurality of transducers and providing a third transducer output signal corresponding to the emitted signal received by the third transducer;

and further comprising

determining a second set of interferometer planes corresponding to a phase difference between the second transducer output signal and the third transducer output signal,

providing output information corresponding to a direction of arrival of the emitted signal relative to the first, second and third transducers, wherein the output information is a function of an intersection of the second set of interferometer planes with a second direction cosine sphere.

14. The method of claim 13 wherein said determining determines said amplitude comparison as a function of a distance D₂₃ between the second transducer and the third transducer.

15. The method of claim 14 wherein the transducers are antennas mounted on a surface of an aircraft.

16. The method of claim 9 wherein said determining determines said amplitude comparison as a function of a distance between two of said plurality of transducers.