Precision geolocation system and method using a long baseline interferometer antenna system

• US 7,286,085 B2
• Filed: 08/11/2005
• Issued: 10/23/2007
• Est. Priority Date: 08/11/2004
• Status: Expired due to Fees

• Current Assignee: Sierra Nevada Corporation
• Original Assignee: Sierra Nevada Corporation
• Inventors: Kolanek, James, Carlsen, Eric
• Primary Examiner(s): PHAN, DAO LINDA
• Application Number:
  US11/201,451
• Publication Number:
  US 20060114157A1
• Time in Patent Office: 803 Days
• Field of Search: 342/417, 342/424, 342/442, 342/450, 342/463, 342/464
• US Class Current: 342/424
• CPC Class Codes: G01S 3/46 using antennas spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems
• CPC Class Codes: G01S 5/04 Position of source determined by a plurality of spaced direction-finders

Abstract

A long baseline interferometer antenna system and method for determining the location of an emitter. The long baseline interferometer antenna system comprises a first antenna, a second antenna, an inertial navigation system, an antenna baseline measurement system, a multi-channel receiver and a processor. The first and second antenna elements are positioned on a platform and are both configured to receive signals from the emitter. The first and second antenna elements form a long baseline antenna pair. The inertial navigation system measures the platform position and attitude; and the antenna baseline measurement system measures the antenna baseline vector between the first and second antenna elements. The multi-channel receiver measures the differential phase between antenna pairs, and the processor computes the emitter location. Additional antenna elements can be included and some can be configured as squinted beam pair and make use of amplitude difference of arrival measurements.

Claims

1. A geo-location method for determining the location of an emitter using a long baseline interferometer antenna system including a first antenna element and a second antenna element mounted on a platform, the first and second antenna elements forming a long baseline antenna pair, the method comprising:

moving the platform along a measurement path;

collecting a series of sets of signal observations from the first and second antenna elements while the platform is moving along the measurement path, each set of signal observations being collected at a particular observation time;

processing the signal observations to provide differential phase measurements between the signal observations of the first and second antenna elements;

collecting platform position and attitude measurements using an inertial navigation system;

interpolating the platform position and attitude measurements to the observation times;

collecting measurements of an antenna baseline vector for the long baseline antenna pair using an antenna baseline measurement system;

interpolating the measurements of the antenna baseline vector to the observation times;

performing a coarse precision emitter location estimate using amplitude difference of arrival measurements; and

performing a fine precision emitter location estimate using phase difference of arrival measurements.

2. The geo-location method of claim 1, further comprising:

collecting a series of signal observations from a third antenna element at the observation times while the platform is moving along the measurement path, the third antenna element being located near the first antenna element, the first and third antenna elements forming a short baseline antenna pair; and

processing the signal observations to provide differential phase measurements between the signal observations of the first and third antenna elements.

3. The geo-location method of claim 2, wherein the step of performing coarse precision emitter location estimate comprises:

generating an initial emitter location estimate; and

generating a coarse emitter location estimate using the initial emitter location estimate.

4. The geo-location method of claim 3, wherein the step of generating an initial emitter location estimate comprises:

measuring the amplitude difference of arrival for the short baseline antenna pair;

measuring the amplitude difference of arrival for the long baseline antenna pair;

estimating the amplitude difference of arrival for the short baseline antenna pair, and for the long baseline antenna pair for several proposed emitter locations; and

calculating the initial emitter location estimate to minimize the difference between the measured amplitude difference of arrivals and the estimated amplitude difference of arrivals at the several proposed emitter locations.

5. The geo-location method of claim 4, wherein the step of generating a coarse emitter location estimate comprises:

starting at the initial emitter location estimate; and

methodically progressing through a plurality of emitter location estimates to find the coarse emitter location estimate, the coarse emitter location estimate being the location estimate of the plurality of emitter location estimates that minimizes the difference between the measured values of the amplitude difference of arrival and the estimated values of the amplitude difference of arrival for the location estimate.

6. The geo-location method of claim 2, further comprising:

performing medium precision emitter location estimate using phase difference of arrival measurements.

7. The geo-location method of claim 6, wherein the step of performing medium precision emitter location estimate comprises:

measuring the phase difference of arrival for the short baseline antenna pair; and

starting at the coarse emitter location estimate; and

methodically progressing through a plurality of emitter location estimates to find the medium emitter location estimate, the medium emitter location estimate being the location estimate of the plurality of emitter location estimates that minimizes the difference between the measured values of the phase difference of arrival for the short baseline antenna pair and the estimated values of the phase difference of arrival for the short baseline antenna pair at the location estimate.

8. The geo-location method of claim 6, wherein the step of performing fine precision emitter location estimate comprises:

measuring the phase difference of arrival for the long baseline antenna pair;

starting at the medium precision emitter location estimate; and

methodically progressing through a plurality of emitter location estimates to find the fine emitter location estimate, the fine emitter location estimate being the location estimate of the plurality of emitter location estimates that minimizes the difference between the measured values of the phase difference of arrival for the long baseline antenna pair and the estimated values of the phase difference of arrival for the long baseline antenna pair at the location estimate.

9. The geo-location method of claim 2, further comprising:

calibrating the geo-location method to reduce the effect of measurement bias errors.

10. The geo-location method of claim 9, wherein the step of calibrating, comprises:

computing the difference between consecutive phase measurements to compute first difference measurements; and

computing the emitter location using the first difference measurements.

11. The geo-location method of claim 9, wherein the step of calibrating, comprises:

solving for the receiver phase bias scalar;

computing the emitter location using the solved value of the receiver phase bias scalar.

12. The geo-location method of claim 9, wherein the step of calibrating, comprises:

solving for the true antenna baseline vector and the antenna baseline bias vector;

computing the emitter location using the solved value of the true antenna baseline vector and the antenna baseline bias vector.

13. The geo-location method of claim 9, wherein the step of calibrating, comprises:

calculating the location of a known emitter using the geo-location method, the known emitter having a known emitter location;

determining the phase bias and the antenna baseline bias from the difference between the calculated location of the known emitter and the known emitter location.