Conical omni-directional coverage multibeam antenna with parasitic elements

• US 5,872,547 A
• Filed: 09/09/1996
• Issued: 02/16/1999
• Est. Priority Date: 07/16/1996
• Status: Expired due to Term

• Current Assignee: Kathrein-Werke KG. (Kathrein SE)
• Original Assignee: Metawave Communications Corp.
• Inventors: Martek, Gary Allen
• Primary Examiner(s): Wong, Don
• Assistant Examiner(s): Ho, Tan
• Application Number:
  US08/711,058
• Time in Patent Office: 890 Days
• Field of Search: 343/700 MS, 343/778, 343/799, 343/815, 343/817, 343/818, 343/846, 343/848, 343/853, 343/890, 343/893, 342/373, 342/374, 342/375
• US Class Current: 343/815
• CPC Class Codes: H01Q 1/246 specially adapted for base stations
• CPC Class Codes: H01Q 1/362 for broadside radiating helical antennas
• CPC Class Codes: H01Q 11/08 Helical antennas
• CPC Class Codes: H01Q 19/10 using reflecting surfaces
• CPC Class Codes: H01Q 19/108 Combination of a dipole with a plane reflecting surface H01Q19/106 takes precedence; strip line H01Q9/065
• CPC Class Codes: H01Q 21/12 Parallel arrangements of substantially straight elongated conductive units travelling-wave antennas comprising transmission line loaded with transverse elements H01Q11/02; Yagi antennas H01Q19/30
• CPC Class Codes: H01Q 21/205 providing an omnidirectional coverage turnstile aerials H01Q21/26
• CPC Class Codes: H01Q 25/00 Antennas or antenna systems providing at least two radiating patterns arrangements for changing or varying the orientation or the shape of the directional pattern H01Q3/00
• CPC Class Codes: H01Q 3/242 Circumferential scanning
• 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: H01Q 9/18 Vertical disposition of the antenna
• CPC Class Codes: H01Q 9/32 Vertical arrangement of element H01Q9/40 takes precedence

Abstract

An omni directional coverage multibeam antenna relief on a ground surface having simple conical shapes to provide beam steering. One advantage of such a system is that the projected area is always constant and broadside to the intended direction resulting in limited scan loss effects. In the case of a cylinder as the conical shape, z-axis symmetry provides a constant antenna aperture projection in any azimuthal direction. Using this geometry, high level, side lobes are reduced considerably because of the natural aperture tapering from dispersion effects. These side lobes are further reduced by the presence of parasitic elements which also result in the added benefit of an increased front and back ratio. This front to back ratio may be further increased by the use of inverted cosine energization of selected antenna elements. Coverage area and power can be controlled by changing the ground surface angle and by selectively activating different antenna beam positions around the circumference of the ground surface, and by selectively changing the phase relationship between a given set of antenna beams.

Claims

1. An antenna system comprising:

a plurality of radiating structures spaced circumferentially around a center point, each radiating structure of said plurality of radiating structures being spaced equidistant from and parallel to a next adjacent radiating structure;

a plurality of passive structures spaced circumferentially around said center point, each passive structure of said plurality of passive structures being spaced equidistant from and parallel to a next adjacent passive structure;

a ground surface circumferentially located around said center point and between said center point and each of said radiating structures, said ground surface also being located between said center point and each of passive structures; and

means for phase shifting a transmission signal from certain activated radiating structures a selected delay amount, the phase shift amount being selected such that the transmission signal wave front leaving said activated radiating structures is in a relatively straight line substantially perpendicular to the direction of travel of said transmission signal, the direction of travel being normal to a point on the ground surface corresponding to one of said activated radiating structures.

2. The antenna system set forth in claim 1 wherein each said radiating structure includes a plurality of individual radiation points.

3. The antenna system set forth in claim 2 wherein certain of said radiation points are dipole antennas.

4. The antenna system set forth in claim 2 wherein certain of said radiation points are patch antennas.

5. The antenna system set forth in claim 2 wherein certain of said radiation points are helical antennas.

6. The antenna system set forth in claim 2 wherein each said passive structure includes a plurality of individual passive elements.

7. The antenna system set forth in claim 6 wherein certain of said passive elements are selected to be a particular size relative to said individual radiation points.

8. The antenna system set forth in claim 7 wherein said particular size is selected to be within the range of sizes from 0% to 20% larger than said individual radiation points.

9. The antenna system set forth in claim 1 wherein said plurality of passive structures are disposed in interleaved fashion with said plurality of radiation structures about said center point.

10. The antenna system set forth in claim 1 wherein said plurality of passive structures is disposed a distance outboard of said plurality of radiation structures, said outboard disposition of said passive structures resulting in a circle defined by said plurality of passive structures being circumferentially located around said center point having a larger radius than a circle defined by said plurality of radiation structures being circumferentially located around said center point.

11. The antenna system set forth in claim 10 wherein said distance is within the range of distances from 0 to 6/16λ

.

12. The antenna system set forth in claim 1 wherein selected ones of said plurality of radiation structures are energized according to an inverted aperture distribution.

13. The antenna system set forth in claim 12 wherein said inverted aperture distribution is an inverted cosine function.

14. The antenna system set forth in claim 12 wherein said inverted aperture distribution is an inverted raised cosine function.

15. The antenna system set forth in claim 12 wherein a radiation pattern illuminated by said system comprises a front to back ratio in excess of 30 dB.

16. The antenna system set forth in claim 12 wherein a frequency is available for multiple reuse by said system, a pattern of said reuse providing for said frequency to be available on two sides of said system displaced radially 180 degrees.

17. The antenna system set forth in claim 1 wherein said phase shift means for each said radiating structure includes first and second delay devices, for establishing a specific phase relationship between respective radiating devices.

18. The antenna system set forth in claim 1 wherein the number of activated radiating structures for any given transmission is selectively controllable.

19. The antenna system set forth in claim 1 wherein the one of said activated radiating structures which is used as the point to measure the direction of wave front travel is selectable.

20. The antenna system set forth in claim 1 wherein the radius of the circumferentially placed radiating structures is λ

/4±

λ

/8 above and normal to the ground surface.

21. The antenna system set forth in claim 1 wherein the spacing between radiating structures is ≧

4/5λ

.

22. The antenna system set forth in claim 1 wherein the ground surface has a top and a bottom edge and wherein each of these edges is rounded inward to form a side lobe suppressor torus.

23. The antenna system set forth in claim 22 wherein at least one of the rounded edges of the ground surface includes signal absorption means.

24. The antenna system set forth in claim 1 wherein the ground surface is at an angle with respect to the vertical.

25. The antenna system set forth in claim 24 wherein the ground surface has a top and a bottom edge and wherein the angle causes the bottom edge of the ground surface to be closer to the center point than the top edge of the ground surface.

26. The antenna system set forth in claim 24 wherein the angle is between 0°

and 45°

from the vertical.

27. The antenna system set forth in claim 24 wherein the angle is selectable from time to time during operation.

28. The antenna system set forth in claim 1 wherein the activation of any one structure involves the activation of at least two adjacent structures.

29. The antenna system set forth in claim 28 wherein said at least two adjacent structures are controlled using Wilkinson and hybrid combiners in a non-interleaved mode with a loss of 3 dB of power.

39. The antenna system set forth in claim 6 wherein each of the passive structures is a series of individual elements.

40. The antenna system set forth in claim 9 wherein said individual elements are of a predetermined size relative to said dipoles, said predetermined size being from the range of sizes from 0% to 20% larger than said dipoles.

30. A selectively directional antenna system comprising:

a plurality of radiating structures spaced circumferentially around a center point;

a plurality of passive structures spaced circumferentially around said center point; and

a ground surface circumferentially located around said center point and between said center point and each of said radiating structures, said ground surface also being located between said center point and each of said passive structures, said ground surface circumscribing a volume substantially perpendicular to a surface upon which signals transmitted from a radiating structure are to be received on.

31. The antenna system set forth in claim 30 wherein ones of said plurality of passive structures are disposed between adjacent ones of said plurality of radiation structures.

32. The antenna system set forth in claim 30 wherein ones of said plurality of passive structures are disposed a distance farther from said ground surface than ones of said plurality of radiation structures.

33. The antenna system set forth in claim 32 wherein said distance is 3/16λ

±

3/16λ

.

34. The antenna system set forth in claim 30 wherein the ground surface is a truncated cone having an angle θ

with respect to the signal receiving surface.

35. The antenna system set forth in claim 34 wherein the angle θ

is variable.

36. The antenna system set forth in claim 30 wherein each of the radiating structures is a series of dipoles spaced parallel to the ground surface and along the longitudinal axis of the ground surface.

37. The antenna system set forth in claim 36 wherein the radiating structures are equidistant from each other.

38. The antenna system set forth in claim 37 wherein the passive structures are equidistant from each other.

41. The antenna system set forth in claim 36 wherein the ground surface forms an angle θ

with respect to the signal receiving surface.

42. The antenna system set forth in claim 30 wherein at least the top or bottom edge of the ground surface forms a curved torus.

43. The antenna system set forth in claim 42 wherein the torus includes lossy material.

44. The antenna system set forth in claim 42 wherein the torus is curved inward.

45. The antenna system set forth in claim 30 wherein the ground surface is discontinuous at at least one point around its circumference.

46. The antenna system set forth in claim 30 wherein each radiating structure is operable from a separate control device.

47. The antenna system set forth in claim 46 wherein each control device is located inboard of its associated radiating structure and connected thereto by a relatively short connection.

48. The antenna system set forth in claim 30 wherein each control device can control the phase of a radiated signal from the associated radiating structure with respect to the phase of the other radiating structures.

49. The antenna system set forth in claim 30 wherein a signal transparent radome covers the antenna system.

50. The antenna system set forth in claim 49 wherein said radome provides support for ones of said plurality of passive structures.

51. The antenna system set forth in claim 30 wherein at least some of the radiating structures are signal receiving structures.

52. The antenna system set forth in claim 51 wherein a signal shield forms two chambers within the volume of the ground surface.

53. The antenna system set forth in claim 52 wherein both chambers are contained within a single radome, all supported by a common mast extending through the longitudinal center of the antenna system.

54. The antenna system set forth in claim 51 wherein one of the chambers contains radiating structures and the other of the structures contains receiving structures.

55. The antenna system set forth in claim 30 wherein certain of the radiating structures have a first design and others of the radiating structures have a second design.

56. The antenna system set forth in claim 30 wherein the radiating structures are bi-directional receiving or transmitting.

57. The antenna system set forth in claim 30 wherein the activation of any one structure involves the activation of four adjacent structures.

58. The antenna system set forth in claim 57 wherein said four adjacent structures are controlled using Wilkinson and hybrid combiners in a non-interleaved mode with a loss of 3 dB of power.

59. The antenna system set forth in claim 57 wherein said four adjacent structures are activated in an inverse aperture distribution.

60. The antenna system set forth in claim 59 wherein said inverse aperture distribution is a cosine function.

61. The antenna system set forth in claim 59 wherein said inverse aperture distribution is a raised cosine function.

62. The antenna system set forth in claim 59 wherein a front to back ratio of a far field radiation pattern of said system is in excess of 30 dB.

63. A method of operating an antenna system having a plurality of radiating structures spaced circumferentially around a center point, each radiating structure spaced equidistant from and parallel to a next adjacent radiating structure, said antenna system also having a plurality of parasitic structures spaced circumferentially around the center point, each parasitic structure spaced equidistant from and parallel to a next adjacent parasitic structure, each parasitic structure also spaced equidistant from and parallel to each radiating structure of a pair of said radiating structures, wherein a ground surface is circumferentially located around the center point and between the center point and each of the radiating structures and the ground surface is also located between the center point and each of the parasitic structures, the method comprising the steps of:

activating ones of said plurality of radiating structures;

delaying a transmission signal from certain of the activated radiating structures a selected delay amount; and

selecting the delay amount such that the transmission signal wave front leaving the activated radiating structures including energy reflected from ones of said plurality of parasitic structures is in a relatively straight line substantially perpendicular to the direction of desired travel of the transmission signal.

64. The method set forth in claim 63 further including the step of dynamically selecting the radiating structures activated for any given transmission.

65. The method set forth in claim 64 further including the step of selecting the one of the activated radiating structures which is used as the point to measure the direction of wave front travel.

66. The method set forth in claim 63 wherein said ones of said plurality of radiating structures are activated utilizing differing energy levels.

67. The method set forth in claim 66 wherein said differing energy levels comprise a raised inverted cosine function.

68. The method set forth in claim 66 wherein said differing energy levels comprise an inverted cosine function.

69. The method set forth in claim 63 wherein the ground surface has a top and a bottom edge and wherein each of these edges is rounded inward to form a side lobe suppressor torus.

70. The method set forth in claim 63 wherein the ground surface has a top and a bottom edge, said method further including the step of positioning the bottom edge of the ground surface to be closer to the center point than is the top edge of the ground surface.

71. The method set forth in claim 63 further comprising the step of:

selecting, during operation, a scan angle in the elevation plane.

72. The method set forth in claim 71 wherein each radiating structure includes a plurality of individual sub-radiating structures, and wherein the step of selecting a scan angle in the elevation plane includes the step of:

adjusting the phase relationship of a signal radiating from the individual sub-radiating structures of each radiating structure.

73. A method of constructing an antenna system comprising the steps of:

establishing a ground surface circumferentially located around a mast, said ground surface circumscribing a volume substantially perpendicular to a surface upon which signals transmitted from a radiating structure are to be received on;

positioning a plurality of antenna structures at spaced intervals circumferentially around the ground surface; and

positioning a plurality of parasitic structures at spaced intervals circumferentially around the ground surface.

74. The method set forth in claim 73 wherein said plurality of parasitic structures are disposed in interleaved fashion with said plurality of antenna structures around the ground surface.

75. The method set forth in claim 73 wherein said plurality of parasitic structures are positioned such that a radius of a circle defined by their positions is a distance greater than a radius of a circle defined by the positions of said plurality of antenna structures.

76. The method set forth in claim 75 wherein said distance is 3/16λ

±

3/16λ

.

77. The method set forth in claim 73 wherein each of said plurality of antenna structures comprises a plurality of dipole antenna elements of predetermined length and each of said plurality of parasitic structures comprises a plurality of individual elements having a size 10%±

10% larger than said dipole antenna elements.

78. The method set forth in claim 73 wherein the ground surface is a truncated cone having an angle θ

with respect to the signal receiving surface.

79. The method set forth in claim 78 further including the step of adjusting the angle θ

in accordance with desired signal receiving surface area coverage.

80. The method set forth in claim 73 further including the step of constructing at least some of the antenna structures as signal receiving structures and some as signal transmission structures.

81. The method set forth in claim 80 further including the step of forming two RF chambers within the volume of the ground surface, one chamber for containing the receiving structures and one chamber containing the transmission structures.

82. The method set forth in claim 81 wherein both chambers are contained within a single radome, all supported by a common mast extending through the longitudinal center of the antenna system.

83. The method set forth in claim 82 further comprising the step of providing support for ones of said plurality of parasitic structures with said radome.

84. The method set forth in claim 73 wherein certain of the radiating structures have a first design and others of the radiating structures have a second design.

85. The method set forth in claim 73 wherein each antenna structure is parallel to the longitudinal axis of the ground surface.

86. The method set forth in claim 85 further including the step of constructing a plurality of individual antenna structures connected to a common signal transmission medium.

87. The method set forth in claim 86 further including the step of adjusting the antenna structures which are connected to a common medium so as to be in phase with each other.

88. The method set forth in claim 87 further including the step of adjusting the antenna structures, which are connected to a common medium so as to be out of phase with each other by a selected amount.

89. The method set forth in claim 73 wherein the activation of any one structure involves the activation of four adjacent structures.

90. The method set forth in claim 89 wherein said activated radiating structures are activated utilizing differing energy levels.

91. The method set forth in claim 90 herein said differing energy levels comprise an inverted cosine function.

92. The method set forth in claim 90 wherein said differing energy levels comprise a raised inverted cosine function.

93. The method set forth in claim 89 wherein said four adjacent structures are controlled using Wilkinson and hybrid combiners in a non-interleaved mode with a loss of 3 db of power.

94. A method of energizing an antenna array to result in a far field radiation pattern having acceptably small side lobes in relation to a main lobe, said antenna array having a plurality of radiating structures spaced circumferentially around a center point, said antenna system also having a plurality of parasitic structures spaced circumferentially around the center point, wherein a ground surface is circumferentially located around the center point and between the center point and each of the radiating structures, and wherein the ground surface is also located between the center point and each of the parasitic structures, the method comprising the steps of:

selecting ones of said plurality of radiating structures to energize, said selected radiating structures being adjacent radiating structures in said plurality of radiating structures, said selected radiating structures forming a sub-array of antenna elements having at least two outer most radiating structures, wherein said sub-array of antenna elements have associated therewith ones of said plurality of parasitic structures; and

energizing said sub-array utilizing a plurality of energy levels, ones of said plurality of energy levels being applied to radiating structures of said sub-array such that a largest energy level is applied to said two outer most radiating structures.

95. The method set forth in claim 94 wherein said plurality of energy levels comprises an inverted cosine function.

96. The method set forth in claim 94 wherein said plurality of energy levels comprises a raised inverted cosine function.

97. The method set forth in claim 94 wherein said far field radiation pattern comprises a front to back ratio in excess of 30 dB.

98. The method set forth in claim 94 wherein said plurality of radiating structures comprises a plurality of individual radiating elements and said plurality of parasitic structures comprises a plurality of individual reflective elements.

99. The method set forth in claim 98 wherein ones of said plurality of reflective elements are selected to be a particular size relative to said individual radiating elements.

100. The method set forth in claim 99 wherein said particular size is selected to be within the range of sizes from 0% to 20% larger than said individual radiating elements.

101. The method set forth in claim 94 wherein said plurality of parasitic structures are disposed in interleaved fashion with said plurality of radiating structures.

102. The method set forth in claim 94 wherein ones of said plurality of parasitic structures are disposed a distance outboard of said plurality of radiating structures, said outboard disposition of said passive structures resulting in a circle defined by said plurality of parasitic structures being circumferentially located around said center point having a larger radius than a circle defined by said plurality of radiating structures being circumferentially located around said center point.

103. The method set forth in claim 102 wherein said distance is within the range of distances from 0 to 3/16λ

.

104. The method set forth in claim 94 further comprising the steps of:

delaying a transmission signal from certain of the energized radiating structures a selected delay amount; and

selecting the delay amount such that the transmission signal wave front leaving the energized radiating structures is in a relatively straight line substantially perpendicular to the direction of desired travel of the transmission signal.