Methods and apparatus for direction of arrival measurement and radio navigation aids

• US 4,975,710 A
• Filed: 08/01/1989
• Issued: 12/04/1990
• Est. Priority Date: 08/01/1989
• Status: Expired due to Term

• Current Assignee: Elie J. Baghdady
• Original Assignee: Elie J. Baghdady
• Inventors: Baghdady, Elie J.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US07/387,761
• Time in Patent Office: 490 Days
• Field of Search: 342/442, 342/433, 342/424
• US Class Current: 342/442
• CPC Class Codes: G01S 3/46 using antennas spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems

Abstract

The disclosure relates to methods, algorithms and apparatus for direction-of arrival (DOA) measurement/computation based on long-baseline, phase-difference, paired-antenna interferometry and on DOA-computing array processing algorithms. Specifically, methods and algorithms based on direct, cyclically unambiguous estimation of the cosine of the DOA are described for resolving the cyclic ambiguities in long-baseline, phase-difference paired-antenna interferometers, and for steering the computations to the vicinities of the solutions in computation-intensive array processing algorithms, thereby reducing computation load and time. The invention enables the design of DOA-determination systems and radio navigation aids that combine desirable characteristics (such as high resolution and accuracy, simpilicity, low cost, self-calibration, etc.) of different methods of extracting/computing DOA data from the outputs of antenna elements that are positioned in diverse arrangements for realizing complementary apertures.

Claims

1. A method of resolving the cyclic ambiguity in the measurement of the phase difference between the outputs of two antennas, responsive to a signal wave charaterized by a wavelength and a direction of propagation relative to the line connecting the positions of said two antennas, and spaced by a known distance such that the product of said distance and the cosine of said direction of propagation, divided by said wavelength, yields a cyclic ambiguity ratio that exceeds unity, comprising the steps of

estimating the cosine of said direction of propagation by a separate means, independent of said measurement;

determining the value of said wavelength by a separate measurement or computation; and

using the results of said estimating and determining to evaluate said ratio.

2. A method of reducing the computational volume and time of a DOA-computing array processing algorithm for determining the direction of propagation of a traveling signal wavefront, comprising the steps of

determining a first estimate of said direction of propagation by means other than said algorithm;

and

using said algorithm to determine an improved estimate of said direction of propagation in the vicinity of said first estimate.

3. A method of determining the cosine of the direction of propagation of a signal wavefront relative to a reference line, comprising the steps of

positioning first two antennas along said reference line separated by a known distance that exceeds a wavelength of said wavefront;

positioning other antennas at points whose positions are known relative to positions of said first two antennas;

measuring the phase difference between the outputs of said first two antennas;

determining a first estimate of said cosine of the direction of propagation by means based on outputs of said other antennas not involving cyclically ambiguous phase difference measurements;

employing said first estimate to compute the cyclic ambiguity ratio that resolves any cyclic ambiguity in the result of said measuring of the phase difference, thus ascertaining an unambiguous measure of said phase difference; and

using said unambiguous measure of said phase difference to determine an improved second estimate of said cosine of direction of propagation.

4. The method of claim 3, wherein said first and other antennas are receiving.

5. The method of claim 3, wherein

said first and other antennas are transmitting;

said wavefront comprises two mutually coherent signal waves at different but commensurable frequencies each of which originates from one of said first two antennas, and a third signal wave that is separable from said two mutually coherent signal waves and originates from said other antennas; and

said steps are carried out at a separate receiving site or platform.

6. A method of determining an estimate of the cosine of the direction of arrival of a traveling signal wavefront of measurable wavelength, comprising the steps of

employing an array of two or more signal-sensing antennas arranged with uniform spacing around the perimeter of a circle;

taking the differences between outputs of diametrically spaced pairs of said antennas;

deriving from said differences between outputs the resultant North-South (NS) signal for the entire said array of antennas;

detecting the amplitude of said resultant NS signal;

detecting the amplitude of the output of any single one of said antennas;

determining the ratio of the amplitude of said resultant NS signal to the amplitude of the output of said single one of said antennas; and

dividing said ratio by the product of one-half of the number of said antennas in the array and π

times the diameter of said circle divided by the wavelength of said signal wave.

7. A method of determining an estimate of the cosine of the radial direction of arrival of a traveling signal wavefront of measurable wavelength, comprising the steps of

employing an array of two or more signal-sensing antennas arranged with uniform spacing around the perimeter of a circle;

taking the differences between outputs of diametrically spaced pairs of said antennas;

deriving from said differences between outputs the resultant East-West (EW) signal and the resultant North-South (NS) signal for the entire said array of antennas;

detecting the amplitude of each of said resultant EW and NS signals;

taking the square of the amplitude of each said resultant EW and NS signals, adding these squares of amplitudes, and then taking the square-root of the resulting sum of said squares;

taking the ratio of the amplitude of said resultant NS signal to said square-root to obtain the cosine of the azimuth angle of arrival of said signal wavefront;

detecting the amplitude of the output of any single one of said antennas;

taking the ratio of said square-root to the amplitude of the output of said single one of said antennas, and dividing this ratio by the product of one-half of the number of said antennas in the array and π

times the diameter of said circle divided by the wavelength of said signal wave, thus obtaining the cosine of the elevation angle of arrival of said signal wavefront; and

multiplying said cosine of the azimuth angle of arrival and said cosine of the elevation angle of arrival to obtain the cosine of said radial angle of arrival.

8. A method of determining an estimate of the cosine of the radial direction of arrival of a traveling signal wavefront of measurable wavelength, comprising the steps of

employing an array of two or more antennas arranged with uniform spacing around the perimeter of a circle, and an additional antenna positioned off said perimeter;

taking the differences between outputs of diametrically spaced pairs of said antennas arranged around said perimeter;

deriving from said differences between outputs the resultant North-South (NS) signal for the entire said array of antennas;

detecting the amplitude of said resultant NS signal;

detecting the amplitude of the output of said additional antenna;

determining the ratio of the amplitude of said resultant NS signal to the amplitude of the output of said additional antenna; and

dividing said ratio by the product of one-half of the number of said antennas on perimeter and π

times the diameter of said circle divided by the wavelength of said signal wave.

9. A method of determining an estimate of the cosine of the radial direction of arrival of a traveling signal wavefront of measurable wavelength, comprising the steps of

employing an array of two or more antennas arranged with uniform spacing around the perimeter of a circle, and an additional antenna at the center of said circle;

taking the differences between the outputs of diametrically spaced pairs of said antennas that are arranged around said perimeter;

deriving from said differences between outputs the resultant NS signal for the entire said array of antennas around said perimeter;

taking the output of said additional antenna and shifting its phase π

/2 radians to obtain its quadrature-phase replica; and

taking the ratio of said resultant NS signal to said quadrature-phase replica and dividing this ratio by the product of one-half of the number of said antennas on perimeter and π

times the diameter of said circle divided by the wavelength of said signal wave.

10. A method of determining an estimate of the cosine of the radial direction of arrival of a traveling signal wavefront of measurable wavelength, comprising the steps of

employing an array of two or more antennas arranged with uniform spacing around the perimeter of a circle, and an additional antenna at the center of said circle;

taking the differences between the outputs of diametrically spaced pairs of said antennas that are arranged around said perimeter;

taking the output of said additional antenna, to be referred to as the center antenna output;

shifting the frequency of one of said resultant NS signal or said center antenna output by a fixed amount, sufficient to make a signal at the unshifted frequency separable completely from a signal at the shifted frequency, to obtain corresponding frequency-shifted signal;

bandpass amplitude-limiting signal corresponding to said resultant NS signal, to obtain signal one;

amplifying signal corresponding to said center antenna output well above the level of signal corresponding to said resultant NS signal, to obtain signal two;

summing said signal two and signal corresponding to said resultant NS signal, to obtain signal three;

amplitude-limiting said signal three, to obtain signal four;

selecting from said signal four only the component centered at the frequency of the signal corresponding to said resultant NS signal, to obtain signal five; and

multiplying said signal one and said signal five, lowpass filtering the result and calibrating the output of said lowpass filtering to read the cosine of said radial direction of arrival.

11. A method of determining an estimate of the cosine of the direction of arrival of a signal wavefront of measurable wavelength, comprising the steps of

employing an array of three or more antennas arranged around the perimeter of a circle;

commutating among the terminals of said antennas to simulate a single antenna in continuous motion around said circle with an angular velocity equal to the frequency of the commutator-clock signal;

detecting the Doppler sinusoidal frequency modulation induced by said simulated antenna continuous motion; and

multiplying said detected Doppler sinusoidal frequency modulation by said commutator-clock signal, lowpass filtering the product and analyzing the result to evaluate a determinant of the direction of arrival of said signal wavefront.

12. The method of claim 11, wherein said multiplying step comprises the steps of setting the phase of said commutator-clock signal to correspond to the phase of said detected Doppler sinusoidal frequency modulation for zero-azimuth, to obtain a zero-azimuth reference-clock signal;

multiplying said zero-azimuth reference clock signal with said detected Doppler sinusoidal frequency modulation, lowpass filtering the product and calibrating the result to read the cosine of the radial direction of arrival of said wavefront.

13. The method of claim 11, wherein said multiplying step comprises the steps of setting the phase of said commutator-clock signal to correspond to the phase of said detected Doppler sinusoidal frequency modulation for zero-azimuth, to obtain a zero-azimuth reference-clock signal;

shifting the phase of said zero-azimuth reference-clock signal π

/2 radians, to obtain a quadrature-azimuth reference-clock signal;

multiplying said zero-azimuth reference-clock signal with said detected Doppler sinusoidal frequency modulation, and lowpass filtering the product to obtain output A;

multiplying said quadrature-azimuth reference clock signal with said detected Doppler sinusoidal frequency modulation, and lowpass filtering the product to obtain output B; and

employing said output A and said output B to determine the direction of arrival of said signal wavefront.

14. The method of claim 13 wherein said employing of said output A and said output B comprises dividing said output B by said output A to obtain the tangent of the azimuth direction of arrival.

15. The method of claim 13 wherein said employing of said output A and said output B comprises applying said output A across one set of cathode-ray tube (CRT) deflection plates, and said output B across the other orthogonal set of CRT deflelection plates, to display the azimuth direction of arrival of said signal wavefront.

16. The method of claim 13 wherein said employing of said output A and said output B comprises

computing the square-root of the sum of the squares of said output A and said output B;

and

calibrating said square-root to read the value of the cosine of the elevation direction of arrival of said signal wavefront.

17. The method of claim 13 wherein said employing of said output A and said output B comprises

computing the square-root of the sum of the squares of said output A and said output B;

and

dividing said output A by said square-root to obtain the cosine of the azimuth direction of arrival (ADOA) of said signal wavefront;

calibrating said square-root to read the value of the cosine of the elevation direction of arrival (EDOA) of said signal wavefront; and

multiplying said cosine of ADOA and said cosine of EDOA to obtain the cosine of the radial direction of arrival (RDOA) of said signal wavefront.

18. A method of estimating the cosine of the radial direction of arrival (RDOA) of a signal wavefront of measurable wavelength, comprising the steps of

employing two antennas spaced by less than said signal wavefront wavelength;

switching abruptly between the terminals of said antennas;

applying the signal output of said switching to a quadrature product demodulator; and

computing the cosine of said RDOA from the lowpass output of said quadrature product demodulator.

19. A method of estimating the cosine of the direction of arrival of a signal wavefront of measurable wavelength, comprising the steps of

providing a set of sensors at different positions in space for intercepting said wavefront;

performing measurements of designated characteristics of the outputs of said sensors taken singly or in combinations;

formulating an algebraic system of simultaneous equations relating the results of said measurements, with trigonometric functions of radial, azimuth and elevation direction angles, and assumed errors in same, as unknowns; and

solving said system of simultaneous equations for said trigonometric functions.

20. The method of claim 19 wherein said solving step comprises

determining a first estimate of the solution to said system of simultaneous equations by means other than said system of equations;

and

utilizing said first estimate so as to initiate iterations of the algrithm for solving said system of equations for successively more refined estimates.

21. An apparatus for resolving the cyclic ambiguity in a direction of arrival determination for a travelling signal wavefront comprising:

means for measuring phase difference between outputs of two antennas, responsive to a signal wave characterized by a wavelength and a direction of propagation relative to a line connecting the positions of said two antennas, and spaced by a known distance such that a product of said known distance and a cosine of said direction of propagation, divided by said wavelength, yields a cyclic ambiguity ratio that exceeds unity;

means for estimating the cosine of said direction of propagation, separately and independently of said measurement;

means for determining the value of said wavelength; and

,

means for evaluating said cyclic ambiguity ratio using the outputs of said means for estimating and said means for determining.

22. An apparatus for reducing the computational volume and time of a DOA-computing array processing algorithm for determining the direction of propagation of a travelling signal wavefront, comprising:

means for determining a first estimate of said direction of propagation by operations other than those of said algorithm; and

,

means for applying said algorithm to determine an improved estimate of said direction of propagation in the vicinity of said first estimate.

23. An apparatus for determining the cosine of the direction of propagation of a signal wavefront relative to a reference line, comprising:

a first antenna means including two antennas positioned along a reference line and separated by a known distance that exceeds a wavelength of a signal wavefront;

a second antenna means including other antennas positioned at points whose positions are known relative to positions of said first two antennas;

means for measuring a phase difference between outputs of said two antennas of said first antenna means to provide a result;

means for determining a first estimate of a cosine of the signal wavefront direction of propagation relative to said reference line by operations on outputs of said other antennas not involving cyclically ambiguous phase difference measurements;

means for applying said first estimate to compute a cyclic ambiguity ratio that resolves any cyclic ambiguity in the result of said measuring of the phase difference, thus ascertaining an unambiguous measure of said phase difference; and

,

means for using said unambiguous measure of said phase difference to determine an improved second estimate of said cosine of direction of propagation.

24. The apparatus of claim 23, wherein said first and second antenna means are receiving antennas.

25. The apparatus of claim 23, wherein:

said first and second antenna means are transmitting antennas;

said signal wavefront includes two mutually coherent signal waves at different but commensurable frequencies each of which originates from one of said first two antennas, and a third signal wave that is separable from said two mutually coherent signal waves and originates from said other antennas; and

,

said means for measuring, means for determining, means for applying and means for using are located at a separate receiving site or platform.

26. An apparatus for estimating a direction of arrival cosine for a travelling signal wavefront of measurable wavelength to determine direction of arrival of said travelling signal wavefront, comprising:

antenna means including an entire array of two or more signal-sensing antennas arranged with uniform spacing around a perimeter of a circle;

means for taking differences between outputs of diametrically spaced pairs of said antennas;

means for deriving from said differences between outputs a resultant North-South (NS) signal for the entire said array of antennas;

means for detecting an amplitude of said resultant NS signal;

means for detecting an amplitude of an output of any single one of said antennas;

means for determining a ratio of the amplitude of said resultant NS signal to the amplitude of the output of said single one of said antennas;

means for dividing said ratio by a product of one-half of the number of said antennas in the array and π

times the diameter of said circle divided by the wavelength of said signal wavefront to produce a cosine value; and

,

means for using said cosine value to determine the direction of arrival of said travelling signal wavefront.

27. An apparatus for estimating the radial direction of arrival cosine of a travelling signal wavefront of measurable wavelength to determine the direction of arrival of said travelling signal wavefront, comprising:

antenna means including an entire array of two or more signal-sensing antennas arranged with uniform spacing around the perimeter of a circle;

means for taking differences between outputs of diameterically spaced pairs of said antennas;

means for deriving from said differences between outputs a resultant East-West (EW) signal and a resultant North-South (NS) signal for the entire said array of antennas;

means for detecting an amplitude of each of said resultant EW and NS signals;

means for taking a square of the amplitude of each of said resultant EW and NS signals, adding these squares of amplitudes, and then taking a square-root of the resulting sum of said squares;

means for taking a ratio of the amplitude of said resultant NS signal to said square-root to obtain a cosine of the azimuth angle of arrival of said signal wavefront;

means for detecting an amplitude of an output of any single one of said antennas;

means for taking the ratio of said square-root to the amplitude of the output of said single one of said antennas, and dividing this ratio by a product of one-half of the number of said antennas in the array and π

times the diameter of said circle divided by the wavelength of said signal wavefront, thus obtaining a cosine of the elevation angle of arrival of said signal wavefront;

means for multiplying said cosine of the azimuth angle of arrival and said cosine of the elevation angle of arrival to obtain the cosine of said radial angle of arrival; and

,

means for using said cosine of said radial angle of arrival to determine the direction of arrival of said travelling signal wavefront.

28. An apparatus for estimating the radial direction of arrival cosine of a travelling signal wavefront of measurable wavelength to determine the direction of arrival of said travelling signal wavefront, comprising:

a first antenna means including an entire array of two or more antennas arranged with uniform spacing around the perimeter of a circle, and a second antenna means including an antenna positioned off said perimeter;

means for taking differences between outputs of diametrically spaced pairs of said antennas arranged around said perimeter;

means for deriving from said differences between outputs a resultant North-South (NS) signal for the entire said array of antennas in said first antenna means;

means for detecting an amplitude of said resultant NS signal;

means for detecting an amplitude of an output of said antenna in said second antenna means;

means for determining a ratio of the amplitude of said resultant NS signal to the amplitude of the output of said antenna in said second antenna means;

means for dividing said ratio by a product of one-half of the number of said antennas on said perimeter and π

times the diameter of said circle divided by the wavelength of said signal wave to produce a cosine value; and

,

means for using said cosine value to determine the direction of arrival of said travelling signal wavefront.

29. An apparatus for estimating the radial direction of arrival cosine of a travelling signal wavefront of measurable wavelength to determine the direction of arrival of said travelling signal wavefront, comprising:

a first antenna means including an entire array of two or more antennas arranged with uniform spacing around the perimeter of a circle, and a second antenna means comprising an antenna at the center of said circle;

means for taking differences between outputs of diametrically spaced pairs of said first antenna means;

means for deriving from said differences between outputs a resultant NS signal for the entire said array of said first antenna means;

means for taking an output of said antenna in said second antenna means and shifting its phase π

/2 radians to obtain its quadrature-phase replica;

means for taking a ratio of said resultant NS signal to said quadrature-phase replica and dividing this ratio by a product of one-half of the number of antennas in said first antenna means and π

times the diameter of said circle divided by the wavelength of said signal wavefront to produce a cosine value; and

,

means for using said cosine value to determine the direction of arrival of said travelling signal wavefront.

30. An apparatus for estimating the radial direction of arrival cosine of a travelling signal wavefront of measurable wavelength to determine the direction of arrival of said travelling signal wavefront, comprising:

a first antenna means including an entire array of two or more antennas arranged with uniform spacing around the perimeter of a circle, and a second antenna means including an antenna at the center of said circle;

means for taking differences between outputs of diametrically spaced pairs of said antennas that are arranged around said perimeter;

means for deriving from said differences between outputs a resultant NS signal for the entire said array of antennas around said perimeter;

means for taking a center antenna output of said antenna in said second antenna means;

means for shifting the frequency of one said resultant NS signal or said center antenna output by a fixed amount, sufficient to make a signal at the unshifted frequency separable completely from a signal at the shifted frequency, to obtain a corresponding frequency-shifted signal;

means for bandpass amplitude-limiting a signal corresponding to said resultant NS signal, to obtain signal one;

means for amplifying a signal corresponding to said center antenna output well above the level of signal corresponding to said resultant NS signal, to obtain signal two;

means for summing said signal two and said signal corresponding to said resultant NS signal, to obtain signal three;

means for amplitude-limiting said signal three, to obtain signal four;

means for selecting from said signal four only a component centered at the frequency of the signal corresponding to said resultant NS signal, to obtain signal five; and

,

means for multiplying said signal one and said signal five, lowpass filtering the result and calibrating the output of said lowpass filtering to read the cosine of said radial direction of arrival.

31. An apparatus for estimating the elevation angle of arrival cosine of a travelling signal wavefront of measurable wavelength to determine the direction of arrival of said travelling signal wavefront, comprising:

a first antenna means including an entire array of two or more signal-sensing antennas arranged with uniform spacing around the perimeter of a circle, and a second antenna means positioned off said perimeter and including an antenna erected vertical to a plane of said circle and two mutually orthogonal antennas laid in said plane, said first and second antenna means receiving a travelling signal wavefront;

means for taking differences between outputs of diametrically spaced pairs of said first antennas means;

means for deriving from said differences between outputs a resultant East-West (EW) signal and a resultant North-South (NS) signal for the entire said array of antennas in said first antenna means;

means for detecting an amplitude of each of said resultant EW and NS signals;

means for taking a square of the amplitude of each of said resultant EW and NS signals, adding the squares of amplitudes, and then taking a square-root of the resulting sum of said squares, to obtain output one;

means for detecting output amplitudes of antennas in said second antenna means, taking squares of said amplitudes, adding said squares of amplitudes, and then taking a square-root of the resulting sum of said squares and multiplying said square root by the product of one-half of the number of antennas in said first antenna means and π

times the diameter of said circle divided by the wavelength of said signal wavefront, thus obtaining output two;

means for taking a ratio of said output one to said output two, and for taking a square root of said ratio to produce a cosine value; and

,

means for using said cosine value to determine the direction of arrival of said travelling signal wavefront.

32. An apparatus for estimating the direction of arrival cosine of a signal wavefront of measurable wavelength to determine the direction of arrival of said signal wavefront comprising:

antenna means including an entire array of three or more antennas arranged around the perimeter of a circle;

means for commutating among terminals of said antennas to simulate a single antenna in continuous motion around said circle with an angular velocity equal to a frequency of a commutator-clock signal;

means for detecting a Doppler sinusoidal frequency modulation induced by said simulated antenna continuous motion; and

,

means for multiplying said detected Doppler sinusoidal frequency modulation by said commutator-clock signal, lowpass filtering the product to provide a result and analyzing the result to evaluate a determinant of the direction of arrival of said signal wavefront.

33. The apparatus of claim 32, wherein the multiplying means further comprises:

means for setting a phase of said commutator-clock signal to correspond to a phase of said detected Doppler sinusoidal frequency modulation for zero azimuth, to obtain a zero-azimuth reference-clock signal;

means for multiplying said zero-azimuth reference clock signal with said detected Doppler sinusoidal frequency modulation, lowpass filtering the product to provide said result and calibrating the result to read the cosine of the radial direction of arrival of said wavefront.

34. The apparatus of claim 32, wherein said multiplying means further comprises:

means for setting a phase of said commutator-clock signal to correspond to a phase of said detected Doppler sinusoidal frequency modulation for zero azimuth, to obtain a zero-azimuth reference-clock signal;

means for shifting the phase of said zero-azimuth reference-clock signal π

/2 radians, to obtain a quadrature-azimuth reference-clock signal;

means for multiplying said zero-azimuth reference-clock signal with said detected Doppler sinusoidal frequency modulation, and lowpass filtering the product to obtain output A;

means for multiplying said quadrature-azimuth reference signal with said detected Doppler sinusoidal frequency modulation, and lowpass filtering the product to obtain output B; and

,

means for employing said output A and said output B to determine the direction of arrival of said signal wavefront.

35. The apparatus of claim 34, wherein said means for employing said output A and said output B further comprises means for dividing said output B by said output A to obtain the tangent of an azimuth direction of arrival.

36. The apparatus of claim 34, wherein said means for employing said output A and said output B further comprises a cathode-ray tube (CRT), with said output A applied across one set of deflection plates, and said output B applied across another orthogonal set of CRT deflection plates, to display an azimuth direction of arrival of said signal wavefront.

37. The apparatus of claim 34, wherein said means for employing said output A and said output B further comprises:

means for computing a square-root of a sum of squares of said output A and said output B; and

means for calibrating said square-root to read a value of the elevation direction of arrival cosine of said signal wavefront.

38. The apparatus of claim 34, wherein said means for employing said output A and said output B further comprises:

means for computing a square-root of a sum of squares of said output A and said output B;

means for dividing said output A by said square-root to obtain a cosine of an azimuth direction of arrival (ADOA) of said signal wavefront;

means for calibrating said square-root to read a cosine value of an elevation direction of arrival (EDOA) of said signal wavefront; and

,

means for multiplying said cosine of ADOA and said cosine of EDOA to obtain the cosine of a radial direction of arrival (RDOA) of said signal wavefront.

39. An apparatus for estimating the radial direction of arrival (RDOA) cosine of a signal wavefront of measurable wavelength to determine the direction of arrival of said signal wavefront, comprising:

antenna means including two antennas spaced by less than a signal wavefront wavelength;

receiver means including a quadrature-product demodulator;

means for switching an input of said receiver means abruptly between terminals of said antennas;

means for applying a signal output of said switching means to said quadrature product demodulator; and

,

means for computing a cosine of a RDOA of said signal wavefront from a lowpass output of said quadrature product demodulator.

40. An apparatus for estimating a cosine of the direction of arrival of a signal wavefront of measurable wavelength comprising:

sensor means including sensors set at different positions in space for intercepting a signal wavefront;

means for performing measurements of designated characteristics of outputs of said sensors taken singly or in combination; and

,

means for formulating an algebraic system of simultaneous equations relating results of said measurements, with trigonometric functions of radial, azimuth and elevation direction angles, and errors in same, as unknowns; and

for solving said system of simultaneous equations for said trigonometric function.

41. The apparatus of claim 40, wherein said means for formulating and solving performs said solving by:

determining a first estimate of a solution to said system of simultaneous equations by means other than said system of equations; and

,

utilizing said first estimate to initiate iterations of an algorithm for solving said system of equations for successively more refined estimates.