Traveling wave interferometry particularly for solar power satellites

• US 4,368,469 A
• Filed: 09/17/1979
• Issued: 01/11/1983
• Est. Priority Date: 09/17/1979
• Status: Expired due to Term

• Current Assignee: Novar Electronics Corp (Honeywell International Inc.)
• Original Assignee: Novar Electronics Corp (Honeywell International Inc.)
• Inventors: Ott, James H., Rice, James S.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US06/075,943
• Time in Patent Office: 1,212 Days
• Field of Search: 343/100 SA, 343/100 ST, 343/854
• US Class Current: 342/352
• 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: H01Q 3/26 varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture H01Q3/12, H01Q3/22, H01Q3/24 take precedence
• CPC Class Codes: H04B 7/185 Space-based or airborne stations; Stations for satellite systemsH04B7/204 takes precedence

Abstract

A method and apparatus for use in scientific measurement analysis and control. Travelling interference fringes are generated by radiating at least two different periodic waves at two different frequencies, one from each of two different radiators. The waves are received, mixed and filtered to detect at least one beat signal from these waves which represents the travelling interference fringe. The phase of that beat signal is detected relative to a reference signal of the same frequency as the beat signal. The radiated waves may be received at a second antenna and the phase of the beat of the waves at the first antenna is compared to the phase of the beat as observed at the second antenna. A third wave may be radiated from the first antenna to provide a reference signal which is the beat generated by the third wave and the other wave from the same radiator.

Claims

1. A method for use in scientific measurement and analysis and comprising:

(a) generating travelling interference fringes by radiating at least two different periodic waves at two different frequencies, one from each of two different radiators;

(b) receiving, mixing and filtering said radiated waves to detect at least one beat signal; and

(c) detecting the phase of said beat signal relative to a reference signal of the same frequency.

2. A method in accordance with claim 1 further comprising receiving, mixing and filtering said waves at at least one other different receiving antenna to detect a second beat signal and wherein said second beat signal is said reference signal.

3. A method in accordance with claim 1 wherein a third wave is also radiated from one of said radiators and wherein said reference signal is a detected beat signal generated by said third wave and the other wave from the same radiator.

6. A method in accordance with claim 5 wherein the steps of claim 2 are repeated for a different pair of sidebands.

4. A method for creating a moving interference fringe pattern and providing a signal which is related to the distance between the fringes, the method comprising:

(a) radiating two periodic waves at two different frequencies, one from one radiator and the other from another radiator;

(b) receiving both of said waves at each of at least two spaced apart receiving antennas;

(c) mixing and filtering the signals which are generated by both of said waves at each of said receiving antennas to detect a beat of said signals; and

(d) detecting the phase difference of each of said beats.

5. A method for creating a moving interference fringe pattern and for providing a signal which is related to the position of said fringes relative to a receiving antenna, the method comprising:

(a) radiating a carrier wave and a sideband wave from a first radiator;

(b) radiating the opposite sideband wave from a second radiator;

(c) receiving, mixing and filtering signals generated by said waves at a receiving antenna to detect a beat of the carrier with each of its sidebands; and

(d) detecting the phase difference of said beats.

7. A method in accordance with claim 5 for also providing a signal related to the distance between said fringes, said method further comprising:

(a) receiving, mixing and filtering signals generated by said waves at a second receiving antenna to detect a beat of said opposite sideband with the signal generated by one of the other waves; and

(b) detecting the phase difference between the beat of said opposite sideband and said one of the other waves as detected for the waves received at each of said antennas.

8. A method in accordance with claim 7 further comprising the steps of:

(a) receiving, mixing and filtering signals generated by said waves at a third receiving antenna positioned non-colinear with said first two receiving antennas to detect the beat of said opposite sideband with the signal generated by said one of the other of said waves; and

(b) detecting the phase difference between the beat of said opposite sideband and said one of said other waves as detected at said third receiving antenna with the corresponding beat as received at said first receiving antenna.

9. A method for generating an electrical signal for use in making a geometrical measurement, said method comprising:

(a) radiating a first sinusoidally varying wave from a first radiator at a first frequency;

(b) radiating a second, sinusoidally varying wave from a second radiator at a second frequency which is different than said first frequency;

(c) receiving both of said waves at each of at least two spaced apart receiving antennas spaced from said first and second radiators;

(d) mixing and filtering the two signals which are generated by said waves arriving at each antenna to produce a beat signal for each of said antennas; and

(e) detecting the phase difference between said beat signals.

10. A method in accordance with claim 9 wherein said waves are electromagnetic waves.

11. A method in accordance with claim 9 wherein said waves are received at three receiving antennas.

12. A method for generating an electrical signal for use in metering the distance between two points in space, said method comprising:

(a) radiating a first, electromagnetic, sinusoidally varying, wave at a first frequency from a first radiator located at one of said points;

(b) radiating a second electromagnetic, sinusoidally varying wave from a second radiator located at the other of said points at a frequency which is different than said first frequency;

(c) receiving both of said waves at each of at least two spaced apart receiving antennas spaced from said points;

(d) mixing the two signals from each of said antennas which are generated by said waves to produce a beat signal for each of said antennas; and

(e) detecting the phase difference between said beat signal.

13. A method in accordance with claim 12 for metering the distance between said two points comprising the further steps of:

(a) detecting the frequency of one of said radiated signals; and

(b) detecting the frequency difference between said radiated signals.

14. A method in accordance with claim 12 comprising:

(a) receiving said waves at a third antenna which is not colinear with said first two antennas;

(b) detecting the phase difference between said beats derived from said radiated waves at said third antenna;

(c) electronically storing data in an electronic computer representing the following parameters;

D_ab =the distance from a first one of said antennas to a second one of said antennas;

D_ac =the distance from said first antenna to the third one of said antennas;

θ

_o =the angle at said first antenna between said second and said third antennas;

θ

₁ =the angle between a line joining said first antenna and said second antenna and the line of intersection between the plane of said antennas and a plane through said first antenna and perpendicular to a line joining said first antenna and said first point in space;

ω

₂ =the radian frequency of the wave from the second of said points in space;

Δ

ω

=the difference in radian frequency between the waves from said points in space;

L=the distance from a first one of said points in space to a first one of said receiving antennas;

c=the velocity of light;

η

=the angle from the zenith of said first receiving antenna relative to the plane of said receiving antennas to said first radiator as observed at said first receiving antenna; and

(d) machine computing the distance d, between said two points in space and θ

_r, the observed orientation of said points, by solving the simultaneous equations;

##EQU11## and wherein Δ

φ

_ab is the total phase difference between the beats described at said first and said second antennas and Δ

φ

_ac is the total phase difference between the beats detected at said first and said third antennas. and wherein

space="preserve" listing-type="equation">Δ

φ

.sub.ab =φ

.sub.ab +m2π

space="preserve" listing-type="equation">Δ

φ

.sub.ac =φ

.sub.ac +n2π

wherein φ

_ab and φ

_ac are the measured values of the above phase shifts respectively.

15. A method in accordance with claim 14 further comprising positioning said first antenna at the apex of a right angle and the others of said antennas on lines forming said right angle.

16. A method in accordance with claim 15 further comprising positioning said other antennas equidistant from said first antenna.

17. A method for generating an electrical signal for compensating the phase of sinusoidally varying waves at the same frequency ω

_T from two points so that they will be in phase along a substantially planar wave front at a receiving location, said method comprising;

(a) radiating a first, sinusoidally varying reference wave from a first one of said points at a first frequency;

(b) radiating a second, sinusoidally varying reference wave from said first point at a second, different frequency;

(c) radiating a third sinusoidally varying wave from said second point at a frequency which is different from the frequency of said two waves from said first point;

(d) receiving, mixing and filtering said reference waves at a location on earth to produce a reference beat signal;

(e) receiving, mixing and filtering one of said reference waves and said wave from said second point at said location on earth to produce a second beat signal; and

(f) detecting the phase difference between said beat signals.

18. A method in accordance with claim 17 wherein one of said reference signals and said signal from said second point are sidebands which are equally spaced on opposite sides of the other of said reference signals.

19. A method in accordance with claim 18 wherein said waves are electromagnetic waves.

20. A method in accordance with claim 19 wherein the lower of said sidebands is ω

_T and wherein the method further comprises the steps of;

(a) electronically storing data in an electronic computer representing the following parameters;

said ω

_T

d=the distance between said points;

L=the distance from a first one of said points in space to a first one of said receiving antennas;

c=the velocity of light; and

(b) machine computing the phase correction angle Δ

φ

_C2 from the following equation;

##EQU12## wherein Δ

φ

_ar is said phase difference.

21. A method in accordance with claim 19 wherein all of said steps of claim 19 are repeated for a different pair of sidebands which are equally spaced on opposite sides of said other reference signal.

22. A method in accordance with claim 21 wherein said method further comprises:

(a) electronically storing data in an electronic computer representing the following parameters;

said ω

_T

d=the distance between said points;

L=the distance from a first one of said points in space to a first one of said receiving antennas;

c=the velocity of light;

ω

_m =the radian frequency of the wave radiated from said second point during radiation of the first pair of said sidebands;

ω

_n =the radian frequency of the wave radiated from said second point during radiation of said different pair of sidebands; and

(b) machine computing the phase correction angle Δ

φ

_C2 from the following equation;

##EQU13## wherein φ

_n is said phase difference between said beat signals for radiation of said second pair of sidebands and wherein φ

_m is said detected phase difference φ

_m between said beat signals for radiation of said first pair of sidebands if the absolute value of said detected phase difference φ

_m less φ

_n is less than π and

wherein otherwise φ

_m is 2π

+φ

_m if φ

_m is less than zero and φ

_m is φ

_m -2π

is not less than zero.

23. A method in accordance with claim 22 further comprising the steps of:

(a) receiving one of said reference waves and said third wave at each of at least two spaced apart receiving antennas spaced from said points;

(b) mixing the two signals from each of said receiving antennas which are generated by said one reference wave and said third wave to produce a beat signal for each of said antennas; and

(c) detecting the phase difference between said beat signals.

24. A method in accordance with claim 23 comprising:

(a) receiving said waves at three antennas which are not colinear;

(b) electronically storing data in an electronic computer representing the following parameters;

D_ab =the distance from a first one of said antennas to a second one of said antennas;

D_ac =the distance from said first antenna to the third one of said antennas;

θ

_o =the angle at said first antenna between said second and said third antennas;

θ

₁ =the angle between a line joining said first antenna and said second antenna and the line of intersection between the plane of said antennas and a plane through said first antenna and perpendicular to a line joining said first antenna and said first point in space;

ω

₂ =the radian frequency of the wave from the second of said points in space;

Δ

ω

=the difference in radian frequency between the waves from said points in space;

L=the distance from a first one of said points in space to a first one of said receiving antennas;

c=the velocity of light;

η

=the angle from the zenith of said first receiving antenna relative to the plane of the receiving antennas to said first radiator as observed at said first receiving antenna; and

(c) machine computing the distance, d, between said two points in space and θ

_r, the observed orientation of said points, by solving the simultaneous equations;

##EQU14## and wherein Δ

φ

_ab is the total phase difference between the beats detected at said first and said second antennas and Δ

φ

_ac is the total phase difference between the beats detected at said first and said third antennas. and wherein

space="preserve" listing-type="equation">Δ

φ

.sub.ab =φ

.sub.ab +m2π

space="preserve" listing-type="equation">Δ

φ

.sub.ac =φ

.sub.ac +n2π

wherein φ

_ab and φ

_ac are the measured values of the above phase shifts respectively.

25. A method in accordance with claim 24 for also aiming and phasing an array of more than three radiating antennas comprising:

(a) radiating said reference waves from a selected reference antenna in said array;

(b) performing the steps of claim 21 to determine a Δ

φ

_C2 for a selected reference antenna and each of the other antennas in sequence, one at a time; and

(c) sequentially correcting the phase of each of said other antennas by its phase correction Δ

φ

_C2 to bring it into the proper phase relative to said selected reference antenna.

40. A method in accordance with claim 20 for additionally avoiding transmission path disturbances by using off-site phase compensation and steering said beam to a second point of incidence, said method further comprising:

(a) performing the steps of claim 20 at a said location which is a first point of incidence on earth spaced a distance D_o from said second point of incidence; and

(b) shifting the wave radiated from each subarray radiator by a phase shift φ

_P for each subarray radiator defined by the expression;

##EQU19## wherein ω

_T represents the frequency of the radiated waves, x represents the distance from a selected one of said subarray radiators to a point which results from the projection of the position of the subarray radiator having the phase of its radiated wave being shifted, onto the plane defined by said first point, said second point and said selected subarray and then projection onto the plane passing through said selected subarray perpendicularly to a line joining said selected subarray and said second point, φ

_c represents the angle between a line joining said first point of incidence with said second point of incidence and a line passing through said first point of incidence and perpendicular to a line joining said secondpoint of incidence and one of said radiators, L represents the distance from said second point of incidence to said one radiator, and c is the speed of light.

41. A method in accordance with claim 40 further comprising the steps of performing the steps of claim 40 in sequence for each of a multiplicity of different locations on earth and determining a corresponding multiplicity of phase correction factors Δ

φ

_C2 and phase shifts φ

_P for each of said locations and then using conventional statistical error reduction techniques for determining a total, optimum phase compensation factor.

42. A method in accordance with claim 22 for additionally avoiding transmission path disturbances by using off-site phase compensation and steering said beam to a second point of incidence, said method further comprising:

(a) performing the steps of claim 22 at a said location which is a first point of incidence on earth spaced a distance D_o from said second point of incidence; and

(b) shifting the wave radiated from each subarray radiator by a phase shift φ

_P for each subarray radiator defined by the expression;

##EQU20## wherein ω

_T represents the frequency of the radiated waves, x represents the distance from a selected one of said subarray radiators to a point which results from the projection of the position of the subarray radiator having the phase of its radiated wave being shifted, onto the plane defined by said first point, said second point and said selected subarray and then projection onto the plane passing through said selected subarray perpendicularly to a line joining said selected subarray and said second point, φ

_c represents the angle between a line joining said first point of incidence with said second point of incidence and a line passing through said first point of incidence and perpendicular to a line joining said second point of incidence and one of said radiators, L represents the distance from said second point of incidence to said one radiator, and c is the speed of light.

43. A method in accordance with claim 42 further comprising the steps of performing the steps of claim 42 in sequence for each of a multiplicity of different locations on earth and determining a corresponding multiplicity of phase correction factors Δ

φ

_C2 and phase shifts φ

_P for each of said locations and then using conventional statistical error reduction techniques for determining a total, optimum phase compensation factor.

26. An apparatus for use in making a geometrical measurement relative to two spaced points, said apparatus comprising:

(a) a first radiator and signal generating means connected thereto for radiating a first periodic wave from a first one of said points at a first frequency;

(b) a second, radiator and signal generating means connected thereto for radiating a second, periodic wave from the second one of said points at a second frequency spaced from said first frequency;

(c) a first receiving antenna spaced from both of said radiators for receiving said waves;

(d) a second receiving antenna spaced from both of said radiators and from said first receiving antenna for receiving said waves;

(e) mixing and filtering means connected to said first and to second receiving antennas for detecting the beat signals of said waves as received at each of said receiving antennas; and

(f) phase detecting means for detecting the phase difference between each of said beat signals.

27. An apparatus in accordance with claim 26 wherein said waves are electromagnetic waves.

28. An apparatus in accordance with claim 26 wherein there is further included:

(a) a third receiving antenna spaced from both of said radiators and spaced from and not colinear with said first and second receiving antennas;

(b) electronic data storage means connected to the output of said phase detecting means for storing data representing at least all but one of the following parameters;

D_ab =the distance from a first one of said antennas to a second one of said antennas;

D_ac =the distance from said first antenna to the third one of said antennas;

θ

_o =the angle at said first antenna between said second and said third antennas;

θ

.sub. = the angle between a line joining said first antenna and said second antenna and the line of intersection between the plane of said antennas and a plane through said first antenna and perpendicular to a line joining said first antenna and said first point in space;

ω

₂ =the radian frequency of the wave from the second of said points in space;

Δ

ω

=the difference in radian frequency between the waves from said points in space;

L=the distance from a first one of said points in space to a first one of said receiving antennas;

c=the velocity of light;

η

=the angle from the zenith of said first receiving antenna relative to the plane of said receiving antennas to said first radiator as observed at said first receiving antenna; and

(c) machine computing means connected to said data storage means for solving at least one of the following simultaneous equations for at least one of said parameters;

##EQU15## wherein;

d=the distance between said two points and

θ

_r =the observed orientation of said points;

and wherein Δ

φ

_ab is the total phase difference between the beats detected at said first and said second antennas and Δ

φ

_ac is the total phase difference between the beats detected at said first and said third antennas. and wherein

space="preserve" listing-type="equation">Δ

φ

.sub.ab =φ

.sub.ab +m2π

space="preserve" listing-type="equation">Δ

φ

.sub.ac =φ

.sub.ac +n2π

wherein φ

_ab and φ

_ac are the measured values of the above phase shifts respectively.

29. An apparatus in accordance with claim 28 wherein said first antenna is positioned at the apex of a right angle and the other of said antennas lie on lines forming said right angle and are equidistant from said first antenna.

30. An apparatus for use in adjusting an array of at least two transmitting antennas to make waves radiated from them at an operating frequency arrive in phase at a receiving antenna means, said apparatus comprising:

(a) means for radiating a first periodic reference wave from a first one of said transmitting antennas;

(b) means for radiating a second, periodic reference wave from said first radiating antenna at a sideband frequency spaced from the frequency of said first reference wave;

(c) means for radiating a third periodic wave from the second one of said transmitting antennas at a second sideband frequency spaced on the opposite side of said second reference wave by a frequency band equal to the spacing of the frequency of said first reference wave from said second reference wave;

(d) a receiving antenna spaced from said transmitting antennas for receiving all of said waves;

(e) mixing and filtering means coupled to said receiving antenna for detecting the beat signal derived from said first reference wave and said second reference wave to provide a reference beat signal and for detecting the beat signal derived from said second reference wave and said third wave; and

(f) phase detecting means for detecting the phase difference between said beat signals.

31. An apparatus in accordance with claim 30 wherein said waves are electromagnetic.

32. A apparatus in accordance with claim 31 wherein the lower of said sidebands is ω

_T and wherein the method further comprises the steps of;

(a) electronically showing data in an electronic computer representing the following parameters;

said ω

_T

d=the distance between said points;

L=the distance from a first one of said points in space to a first one of said receiving antennas;

c=the velocity of light; and

(b) machine computing the phase correction angle Δ

φ

_c2 from the following equation;

##EQU16## wherein Δ

φ

_ar is said phase difference.

33. An apparatus in accordance with claim 32 wherein there is further included:

(a) means for radiating a different pair of sideband frequencies from said transmitting antennas;

(b) electronic data storage means connected to the output of said phase detecting means for storing the following parameters;

said ω

_T

d=the distance between said points;

L=the distance from a first one of said points in space to a first one of said receiving antennas;

c=the velocity of light;

ω

_m =the radian frequency of the wave radiated from said second point during radiation of the first pair of said sidebands;

ω

_n =the radian frequency of the wave radiated from said second point during radiation of said different pair of sidebands; and

(c) machine computing means connected to said data storage means for solving the following equation;

##EQU17## wherein φ

_n is said phase difference between said beat signals for radiation of said different pair of sidebands and wherein φ

_m is said detected phase difference φ

_m between said beat signals for radiation of said first pair of sidebands if the absolute value of said detected phase difference φ

_m less φ

_n is less than π and

otherwise φ

_m is 2π

+φ

_m if φ

_m is less than zero and φ

_m is φ

_m -2π

if φ

_m is not less than zero.

34. An apparatus in accordance with claim 32 or 33 wherein there is further provided:

(a) a second receiving antenna spaced from said first receiving antenna;

(b) a third receiving antenna spaced from and not colinear with said first and said second receiving antennas;

(c) mixing and filtering means connected to each of said receiving antennas for detecting the beat signals derived from the beat of one of said reference waves and said third wave as received at each of said receiving antennas; and

(d) phase detecting means for detecting the phase difference between said beat signals.

35. A method for phase compensating sinusoidally varying waves at the same frequency, ω

_T, from at least two points so that they will be substantially focused to constructively reinforce at a single point at a receiving location, said method comprising;

(a) Radiating a first, sinusoidally varying reference wave at a frequency different from ω

_T from a reference point;

(b) Radiating a second sinusoidally varying reference wave from said reference point at a second frequency which is different from ω

_T and from said first wave;

(c) Radiating a third sinusoidally varying wave from one of said two points at a frequency of ω

_T ;

(d) Receiving, mixing and filtering said reference waves at a location on earth to produce a reference beat signal;

(e) Receiving, mixing and filtering one of said reference waves and said wave from one of said two points at said location on earth to produce a second beat signal;

(f) Detecting the phase difference between said beat signals;

(g) Shifting the phase of the third sinusoidally varying wave by a phase angle equal to said detected phase difference between said beat signals so that the phase difference between said beat signals will become zero; and

(h) Repeating steps (c) through (g) for a wave radiated at a frequency ω

_T from the second one of said two points.

36. A method in accordance with claim 35 wherein said waves are electromagnetic waves.

37. A method in accordance with claim 35 wherein one of said reference waves and ω

_T are sidebands which are equally spaced on opposite sides of the other said reference signals.

38. A method in accordance with claim 36 wherein all said steps of claim 37 are repeated for a different pair of sidebands which are equally spaced on opposite sides of said other reference signal.

39. A method for steering a beam of radiated waves which is radiated from a plurality of spaced subarray radiators forming a radiating antenna field, from incidence upon a first point with a planar wave front to incidence upon a second point with a planar wave front, said method comprising:

shifting the wave radiated from each subarray radiator by a phase shift φ

_P for each subarray radiator defined by the expression;

##EQU18## wherein D_O represents the distance between said points of incidence, ω

_T represents the frequency of the radiated waves, x represents the distance from a selected one of said subarray radiators to a point which results from the projection of the position of the subarray radiator having the phase of its radiated wave being shifted, onto the plane defined by said first point, said second point and said selected subarray and then projection onto the plane passing through said selected subarray perpendicularly to a line joining said selected subarray and said second point, θ

_c represents the angle between a line joining said first point of incidence with said second point of incidence and a line passing through said first point of incidence and perpendicular to a line joining said second point of incidence and one of said radiators, L represents the distance from said second point of incidence to said one radiator, and c is the speed of light.

44. A method for phase adjusting the subarray radiators of an antenna array while the array is radiating at a primary operating frequency, said method comprising:

(a) radiating a wave from a subarray radiator at a frequency which is spaced from said primary operating frequency;

(b) comparing the phase of said wave to the phase of a reference signal at the same frequency as a signal derived from said wave to determine the phase difference;

(c) calculating a phase compensation angle for said subarray which will bring the radiation from said subarray into a selected phase relationship with the radiation from said array at said operating frequency;

(d) adjusting the phase of said subarray by said phase compensation angle; and

(e) repeating said steps (a) through (d), in sequence, for others of said radiators.