Combined phase-circle and multiplatform TDOA precision emitter location

• US 5,914,687 A
• Filed: 06/01/1998
• Issued: 06/22/1999
• Est. Priority Date: 06/01/1998
• Status: Expired due to Fees

• Current Assignee: Litton Systems Incorporated
• Original Assignee: Litton Systems Incorporated
• Inventors: Rose, Conrad M.
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US09/088,258
• Time in Patent Office: 386 Days
• Field of Search: 342/156, 342/417, 342/424, 342/442, 342/450
• US Class Current: 342/442
• CPC Class Codes: G01S 2205/03 Airborne
• CPC Class Codes: G01S 5/0244 Accuracy or reliability of position solution or of measurements contributing thereto
• CPC Class Codes: G01S 5/0249 Determining position using measurements made by a non-stationary device other than the device whose position is being determined
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Abstract

A method for determining the geolocation--i.e., the latitude, longitude, and altitude--of a stationary emitter emitting an RF signal. The method employs at least one moving observer to measure electrical phase change of the emitter over two or more successive dwell intervals, and at least two observers, moving or stationary and of known position, to determine the pulse time of arrival of the emitter signal. The phase change measurements are taken using a long baseline interferometer (LBI), and the pulse time of arrival measurements are calculated using short baseline interferometers (SBI). Circles of position are generated from bearing change measurements ascertained from the LBI phase change measurements, and hyperbolic lines of position are generated based on the SBI measurements. The position of the emitter is then determined from the intersection of the circles and lines of position.

Claims

1. A method for determining the geolocation of a stationary emitter, the method comprising the steps of:

measuring using a long baseline interferometer (LBI) the ambiguous electrical phase change of the emitter signal corresponding to the change in signal angle of arrival (AOA) due to observer movement with respect to the emitter;

resolving the ambiguous electrical phase change to determine the electrical phase measurement from the ambiguous set that is uniquely associated with the AOA or bearing change;

utilizing the electrical phase measurement to calculate the bearing change of the observer;

creating circles of position (COPs) along which the emitter must lie based on the bearing change;

calculating the time difference of arrival (TDOA) of the emitter RF signal received by at least two observers of known position;

generating a hyperbola along which the emitter must lie based on the TDOA calculations from the at least two observers; and

determining the intersection of the COPs and hyperbola to arrive at a distinct point of location.

2. The method of claim 1, further comprising the steps of:

using short baseline interferometers (SBIs) positioned on each of at least two observers to measure the angle of arrival (AOA) of the signal from the emitter;

obtaining preliminary coarse location to the emitter based on the intersection of the AOA measurements from the at least two observers; and

computing an optimum position for the at least two observers based on phase circle and TDOA geometry from the preliminary coarse location.

3. The method of claim 1, said creating step further comprising the steps of:

resolving the LBI electrical phase change ambiguity by determining AOA at both the start and finish times of the LBI electrical phase change measurement using at least one short baseline interferometer (SBI);

measuring emitter polarization at both the start and finish times of the LBI electrical phase change measurement;

predicting the emitter polarization error present in the LBI electrical phase difference measurement based on the emitter polarization measurements and SBI AOA measurements; and

adjusting the COPs based on the predicted emitter polarization error.

4. The method of claim 1, said generating step further comprising utilizing location of the emitter by at least one SBI to verify that each of the at least two observers is measuring an identical pulse of the emitter RF signal.

5. The method of claim 1, wherein said measuring step and said calculating step are performed using the same one of the at least two observers.

6. The method of claim 1, wherein said calculating step is performed by two stationary observers, or one moving and one stationary observer.

7. A method for determining using a first moving observer and a second observer, the geolocation of a stationary emitter, the method comprising the steps of:

measuring, using a long baseline interferometer (LBI), the ambiguous electrical phase change caused by the bearing change between successive dwell intervals of the first observer with respect to the emitter;

taking phase measurements of the emitter signal over the successive dwell intervals using a short baseline interferometer (SBI);

resolving the differential phase ambiguity present in the LBI phase change measurements by comparison to the unambiguous phase measurements taken by the SBI;

recording the position of the first observer and the spatial location of the LBI at each dwell interval;

performing pulse time-of-arrival (TOA) measurements at the first and second observers during predetermined clock intervals;

forming time-difference-of-arrival (TDOA) measurements using the TOA measurements of identical pulses of the emitter signal;

generating circular lines of position (LOPs) and hyperbolic LOPs, the circular lines of position being generated from the bearing change measurements of the LBI resolved by the SBI phase measurements, and the hyperbolic LOPs being generated from the TDOA measurements; and

determining the intersection point of the circular and hyperbolic LOPs to arrive at a distinct point of location of the emitter.

8. The method of claim 7, wherein said generating step is executed prior to said performing step, and the second observer is in motion.

9. The method of claim 8, wherein

the circular LOPs intersect to provide two possible emitter locations, the correct location being determined using the unambiguous phase measurements taken by the SBI;

and

the geolocation estimate provided by the intersected COP'"'"'s is then used to predict the optimum observer positions for performing a TOA measurement resulting in the most orthogonal COP and TDOA LOP intersection.

10. The method of claim 9, further comprising the step of verifying the TDOA measurement using the geolocation estimate.

11. The method of claim 10, said verifying step comprising the step of checking that each of the at least two observers is measuring an identical pulse of the emitter RF signal, said checking step comprising:

predicting a time window within which the pulses received by the second observer and subsequent observers must lie, wherein

the time window is less than the pulse repetition interval of the emitter signal, and is offset in time for each of the second and subsequent observers with respect to the first observer based on the predicted distance of each observer from the emitter location estimated by the intersecting COPs.

12. The method of claim 7, wherein the successive dwell intervals are separated by between one-half second and four seconds.

13. The method of claim 7, wherein said measuring step comprises employing phase detection circuitry designed so that, for the AOA derived from said phase measurement, the AOA measurement error is accurately characterized by the RF carrier frequency and signal-to-noise ratio (SNR) of the emitter signal.

14. The method of claim 7, wherein the circuitry for measuring said TOA is such that the TOA measurement error is accurately characterized by the signal pulse width, pulse rise time, and signal-to-noise ratio (SNR).

15. The method of claim 7, wherein said recording step comprises the step of utilizing a navigation system and association means.

16. The method of claim 7, further comprising the steps of:

extracting the parameters of emitter signal pulse width, pulse rise time, frequency, and amplitude; and

applying the parameters in order to

estimate the signal-to-noise ratios (SNRs) of the TOA measurements and of the bearing change measurements resolved by the phase measurements of the SBI; and

compute the error variances in the TOA and phase measurements.

17. The method of claim 16, said determining step further comprises the steps of:

assessing the accuracy of the LOPs based on the error variances computed; and

using the error variances, further adjusting the determined LOP intersection point to obtain the minimum-variance estimate or minimum-error estimate of emitter location, the minimum-variance estimate and minimum-error estimate constituting the estimate that statistically minimizes the difference between the predicted phase and predicted TOA measurement values based on the intersection point, and the actual measured phase and TOA.