Multiplatform ambiguous phase circle and TDOA protection emitter location

• US 5,999,129 A
• Filed: 06/01/1998
• Issued: 12/07/1999
• Est. Priority Date: 06/01/1998
• Status: Expired due to Fees

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated
• Inventors: Rose, Conrad M.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US09/088,196
• Time in Patent Office: 554 Days
• Field of Search: 342/394, 342/387, 342/442
• US Class Current: 342/394
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Abstract

A method and system for determining the geolocation--i.e., the latitude, longitude, and altitude--of a stationary RF signal emitter from two or more moving observer aircraft. The observers receive signals from the emitter and the system measures the phase difference between the signals. The observers then perform pulse time of arrival (TOA) measurements over a predetermined clock interval, and calculate the time difference of arrival (TDOA) of corresponding, same-pulse, emitter signals. Based on geometric relationships, the system creates a series of circular lines of position (LOPs) for each observer, and computes hyperbolic LOPs based on the TDOA calculations. The system determines emitter location from the intersection of the hyperbolic LOPs and the circular LOPs.

Claims

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

receiving first and second emitter signals, respectively, at the first and second moving observers;

measuring the ambiguous phase difference between the first and second signals at corresponding update intervals;

estimating the greatest and least possible integer value of the ambiguous phase difference, the integer values comprising a set of possible ambiguity integers;

performing pulse time-of-arrival (TOA) measurements of the emitter signal received by the observers over a predetermined clock interval;

using the TOA measurements performed by the observers to calculate the time-difference-of-arrival (TDOA) of corresponding, same-pulse, emitter signals;

generating a family of circular lines of position (LOPs) for each observer based on the ambiguous phase differences measured and the integer values estimated, wherein with no measurement error the emitter would lie on exactly one of the circular LOPs associated with each observer;

computing hyperbolic LOPs based on the TDOA calculations; and

determining emitter location utilizing the intersection of the hyperbolic LOPs generated from the TDOA measurement, and circular LOP data.

2. The method of claim 1, said determining step comprising selecting the emitter location represented by the common intersection of the single circular LOPs, on which the emitter must lie in the absence of measurement error, from each family of circular LOPs associated with each observer, and a limb of the hyperbolic LOP on which, in the absence of measurement error, the emitter must lie.

3. The method of claim 1, said generating step comprising the step of bounding the set of possible ambiguity integers by making a preliminary estimate of coarse location of the emitter, and using only ambiguity integers that generate phase circles intersecting an error ellipse associated with the coarse location estimate.

4. The method of claim 3, further comprising the step of comparing the amplitudes of the signal direction of arrival measurements made on each of the at least two moving observers.

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

employing the determined emitter location to predict the direction of arrival (DOA) of the emitter signals associated with each ambiguous phase difference measurement;

refining the ambiguity integer estimates based on the DOA predictions; and

differentially resolving each ambiguous phase difference measurement.

6. The method of claim 5, further comprising the steps of deriving emitter elevation from the direction of arrival predictions and utilizing the emitter elevation data to correct coning errors associated with said making step.

7. The method of claim 6, further comprising the step of adjusting the ambiguous phase difference measurements using the direction of arrival data and polarimeter measurements made at each ambiguous phase measurement to correct for phase difference measurement bias errors caused by changes in the emitter signal polarization.

8. The method of claim 7, wherein system measurement errors create a plurality of possible common intersections, said method further comprising the steps of:

applying a maximum likelihood estimator to process the adjusted ambiguous phase difference measurements to generate a corresponding set of refined estimated emitter locations; and

choosing from the refined estimated emitter locations the unique one for which the difference between the phase and TDOA measurements predicted by the refined estimated location, and the actual adjusted respective phase and TDOA measurements associated with that location, form a sequence exhibiting the least statistical bias and the least sample-to-sample statistical correlation.

9. A system to geolocate a stationary emitter and comprising, as a minimum, two moving observers, both of whom measure the ambiguous phase change of the emitter between two positions on each of their flight paths, and two observers, possibly stationary or possibly the same observers performing the phase measurements, to measure emitter same-pulse time-of-arrival, comprising on each moving observer

first and second antennas for generating first and second emitter detection signals containing ambiguous phase information,

phase difference detection circuitry and memory to store the ambiguous phase thus detected between emitter updates, these updates typically being from one half to several seconds apart,

means to difference these stored and ambiguous phase differences and

means to estimate the largest and smallest possible integer value of the phase change ambiguity,

a navigation system and association means providing the moving observer position at the start and end of the emitter update measurement, and the spatial location of the first and second antenna,

and comprising on the possibly stationary observers,

a clock on each observer having a one day stability of at least 10^-11 second per day,

means to adjust these clocks on two observers so that they are in temporal phase with one another,

a data link to command the second observer to perform a pulse time-of-arrival (TOA) measurement during a predetermined clock interval,

TOA measurement means on each observer,

means to form the time-difference-of-arrival (TDOA) from these same-pulse TOA measurements,

and including at a site possibly distinct from any observer, but data linked to the observers,

computing means to derive initial emitter geolocation from the TDOA and phase-circle LOP estimates,

including means to measure received signal amplitude on two or more antennas to determine the correct coarse location from a set of statistically equally likely estimates,

means to measure the signal direction of arrival from the observer position at each phase measurement update and the initial emitter position estimate,

means to predict the LBI phase from the estimated DOA and known LBI baseline position,

means to employ this predicted phase to differentially resolve all the LBI ambiguous phase measurements between the first and final moving observer positions simultaneously for both observers,

means to cone correct the measured resolved phase using the elevation found from the estimated DOA,

a polarimeter to measure emitter polarization during the LBI phase measurement,

calibration means to remove polarization induced phase errors from the resolved and cone corrected measured phase using a calibration table where the phase calibration data in the table is a function of DOA and emitter polarization, and is accessed using the computed DOA and measured polarization,

computing means to rederive emitter geolocation from the TDOA and cone phase-circle LOP estimates generated from the corrected phase data,

predictive means employing this refined location to verify the pulse TOA measured at each relevant observer is the same pulse from the same emitter, and

corrective means to remeasure TDOA if it is not.

10. A system as in claim 9, where the emitter polarization is obtained from phase and amplitude measurements using a dual polarized antenna element, this antenna forming one element in the LBI array, comprising

a receiver controlled switch at the dual antenna element to chose the same polarization as the second antenna element of the long baseline interferometer when making LBI phase measurements, and to allow during the same receiver dwell

the simultaneously measurement of the dual antenna right and left polarization phase and amplitude response, with

memory to stored these measurements, along with the observer position and attitude (NAV data) when the measurement was made, and

means to subsequently generate emitter direction of arrival by combining the emitter coarse location with this stored NAV data, and so, based on the dual polarization phase and amplitude measurements, find the emitter polarization during the receiver dwell during which the LBI phase measurement was made.

11. A system as in claim 9 where generating the ambiguous set of phase-circles at each observer measuring LBI phase differences comprises bounding the LBI differential phase ambiguity integer set, utilizing

observer altitude obtained from the NAV system at each of the LBI phase measurements, from which the maximum possible range to the emitter, or radar horizon, is found,

the angular region relative to the LBI baseline in which the emitter can be detected when on the radar horizon,

the angular region relative to the LBI baseline in which the emitter can be detected when at the closest assumed range from the observer,

observer attitude and position obtained from the NAV system at each of the LBI phase measurements,

means to determine the LBI antenna spatial locations from this position and attitude data at the phase measurement updates, and hence to determine the LBI baseline spatial position,

means to determine, by postulating a uniform emitter distribution in the largest region determined from the radar horizon, minimum emitter range, and angular detection boundaries, and from the LBI baseline spatial position, the minimum and maximum ambiguity integer possible,

association of a unique phase circle with each separate phase difference from the set of measured phase differences resolved by each integer between, and including, the maximum and minimum possible integer values.

12. A system as in claim 9 where the means to employ predicted phase obtained from the emitter location to differentially resolve all the LBI ambiguous phase measurements between the first and second moving observer positions simultaneously for both observers includes means to determine the correct emitter position estimate from a set of possible locations, where each estimate in this set of possible locations is initially determined to be statistically equally likely, before correcting the ambiguous phase measurements for bias errors caused by antennas being squinted, i.e. not having a common boresite, this system comprising

generating a set of predicted LBI differential phase changes for each actual LBI differential phase measurement, using each possible emitter location, observer position and observer attitude during the LBI phase measurements,

forming test sets of resolved LBI differential phase measurements, each test set formed by resolving all LBI differential phase measurements from the set of predicted phases associated with a possible emitter location, and forming all such sets for all equally likely location estimates,

generating sets of azimuth estimates from the emitter and aircraft positions, and each phase test set,

utilizing these sets of azimuth measurements to access a set of stored phase correction factors, which correction factors depend on signal DOA, and to apply these correction factors to the corresponding phase measurements to reduce the effects of polarization and elevation errors due to antenna squint,

generating a new set of azimuth measurements from this set of corrected phase measurements,

deriving the maximum likelihood estimate from the new azimuth estimates comprising a set associated with each possible emitter position,

computing the variance of the emitter locations with the new azimuth estimates utilizing the well known theoretical properties of the maximum likelihood estimator,

choosing the unique emitter location as the site associated with the statistically closest match between azimuth measurement errors predicted from this variance, and the azimuth errors actual measured.