CA1147851A - Slot array antenna with amplitude taper across a small circular aperture - Google Patents

Slot array antenna with amplitude taper across a small circular aperture

Info

Publication number
CA1147851A
CA1147851A CA000361419A CA361419A CA1147851A CA 1147851 A CA1147851 A CA 1147851A CA 000361419 A CA000361419 A CA 000361419A CA 361419 A CA361419 A CA 361419A CA 1147851 A CA1147851 A CA 1147851A
Authority
CA
Canada
Prior art keywords
slots
circular aperture
resonators
slot array
rectangular waveguide
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA000361419A
Other languages
French (fr)
Inventor
George D.M. Peeler
Chester J. Hunt
Richard J. Conti
Ninalbo G. Damocogno
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Raytheon Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Raytheon Co filed Critical Raytheon Co
Application granted granted Critical
Publication of CA1147851A publication Critical patent/CA1147851A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/22Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/0006Particular feeding systems
    • H01Q21/0037Particular feeding systems linear waveguide fed arrays
    • H01Q21/0043Slotted waveguides
    • H01Q21/005Slotted waveguides arrays

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Waveguide Aerials (AREA)

Abstract

SLOT ARRAY ANTENNA WITH AMPLITUDE TAPER
ACROSS A SMALL CIRCULAR APERTURE

Abstract of the Disclosure A small slot array antenna with a circular aperture and linear polarization is shown to be made up of a plurality of slotted waveguides having different lengths and different widths. The slots in the waveguides are positioned to optimize amplitude taper in any plane passing through the center of the array normal to the surface thereof and to maximize the number of such slots.

Description

Backqround of the Invention This invention pertains generally to antennas for radio frequency energy and particularly to antennas wherein à planar array of slotted waveguides is used.
It has been common practice in the art of designing radar antennas for seekers in guided missiles to use a so-called resonant slot array. According to known practice, such an array is formed by mounting a plurality of similarly dimensioned slotted rectangular waveguides in proximity with one another to cover a predetermined aperture. An electrical short circuit is formed across one end of each waveguide to make a resonant structure wherein standing waves may exist to optimize the energization of the slots. A corporate feed of conventional design then is connected to the second ends of the waveguide to allow operation of the resonant slot array either as a trans-mitting antenna or a receiving antenna, such as a monopulse antenna.
Ordinarily, when a resonant slot array is to be used in a guided missile, it is necessary that: (1) a broadside pencil beam be formed so that antenna gain is maximized, with sidelobe levels a~ low as possible; and (2) the energy in the beam be linearly polarized, with cross-polarization effects minimized.
In order to achieve the foregoing in the limited space available in the cylindrical body of a guided missile, the aperture of the usual slot array is circular in shape, the array itself is -4'~q~l,5l1f mounted so as to be steerable in y~ and a~lmu~h and the orien-S119 tation of all of the slots with respect to the longitudinal axes ~1/1s of the waveguides is maintained constant. Further, if the slot array is to be operated as a monopulse antenna, the number of waveguides and disposition of slots is such that an equal number - 1 ~

8~1 of slots is located in each quadrant of the aperture. In addition, the constraints on any slot array which must be met to avoid grating lobes or reduction in efficiency must be observed. That is to say, for a given frequency of operation, proper attention must be given to the dimensions of the wave-guides, the spacing between slots and the position of the electrical short circuit in each one of the waveguides. Thus, in a typical application wherein the aperture of an antenna in a guided missile may have a diameter of S", a slot array for X-band may have a maximum of 20 slots when known techniques are used to design such an array. Because the antenna gain of any slot array is directly related to the number of slots, the antenna gain of the array is limited.
Another problem is encountered with the conventional slot array wherein similarly dimensioned waveguides are used.
Because the positions of the slots in each waveguide (along the length of such guide) are fixed, it is difficult to produce a symmetrical pencil beam. As a result, the quality of performance of the conventional slot array varies, depending upon the direc-tion of a target from boresight.

785~L
Summary of the Invention In view of the foregoing background of this invention, it is a pri-mary object hereof to provide a slot array wherein, with a circular aperture, the number of slots may be increased beyond the largest number possible when known techniques are applied in the design of such an array.
Another object of this invention is to provide a slot array which incorporates a larger number of slots than heretofore deemed possible in a cir-cular aperture and at the same time may be used as a monopulse antenna.
Still another object of this invention is to provide an improved slot array wherein the spacing between slots may be optimized to produce a symmetrical pencil beam.
The foregoing and other objects of this invention are attained gen-erally by providing, in a resonant slot array having a circular aperture, a plurality of differently dimensioned slotted rectangular waveguides disposed in proximity with one another to form the circular aperture, the spacing be-tween the slots and the position of the requisite electrical short circuit in each one of such waveguides being determined by a selected dimension of each wavegulde.
In accordance wlth the present invention, there is provided a linear-ly polarlzed slot array antenna having a substantially circular aperture, the ratio between the diameter of such aperture and the wavelength of radio fre-quency energy at the design frequency of such antenna being in the order of 5:1, such antenna comprising: (a2 a first plurality of rectangular waveguide resonators dimensioned, when ~ux~aposed with narrow walls abutting, substan-tially to cover a first half of the circular aperture, the width of the broad wall of each successive one of such waveguide resonators decreasing outwardly from the centrally located one of such waveguides; (b) a second like plurality of rectangular waveguide re~onator~ covering the second half of the circular aperture; and (c? a plurality of radiating slots formed through the broad wall of each one of the rectangular waveguide resonators, such slots being parallel one to another with the center of each different slot lying in a plane of maximum electric field within its corresponding rectangular waveguide resonator, ~, .: ~

., .,~

~7~5~

the distances of such slots in each such resonator from the center-line thereof increasing from the center to each end of such resonator to provide amplitude taper along the length of such resonators.

- 3a -:

~4785~ `

srief Description of the Drawings For a more complete understanding of this invention, reference is now made to the following description of the accompanying drawing wherein the single Figure is a plan view of an antenna according to this invention.

~7~5~

Description of the Preferred Embodiment Referring now to the FIGURE, the disposition of slots (numbered below) in waveguides lOu, 12u, 14u, 141, 121 and 101 of an exemplary resonant slot array (intended for use at X-band in a monopulse radar in a guided missile where a largest allow-able aperture 11 is circular in shape with a diameter of 5") is shown. Because the slots in waveguides 101, 121 and 141 are disposed, respectively, in the same way as the slots in wave-guides lOu, 12u and 14u, and because the dimensions of similarly numbered waveguides are the same, only the latter waveguides will be described. Also, the thickness of each wall in each waveguide and the conventional corporate feed needed have not been shown.
Starting with waveguide 14u, the width W14 (meaning the inslde dimension of the broad wall of a rectangular waveguide) , i9 cho~en so that the cutoff frequency of the dominant TEol mode in such guide here is near the low end of X-band. The thickness (not shown but meaning the inside dimension of the narrow wall of a rectangular waveguide) is chosen so that the cutoff frequency of the next higher mode (the TElo or TE20 - mode) is above the highest frequency in the X-band. Here a conventional rectangular waveguide (having inside dimensions of 0.900" x 0.400") for use at X-band is employed.
It will be recognized that the waveguide wavelength of - X-band energy within waveguide 14u is longer than the wave-length of such energy in free space and that the slots must be spaced at distances determined by the waveguide wavelength.
Even so, with an aperture 5" in diameter, with shunt slots it is ,~ still possible here to have six slots spaced at half-wavelengths ~- 30 (measured in the waveguide along the axis 14u) and an electrical 35~

short circuit spaced one-quarter wavelength from the last slot (say slot 14u(3')).
Slots 14u(3), 14u(1) and 14u(2') are spaced from each other at intervals of one wavelength along the axis 14u. Similarly, slots 14u(2), 14u(1') and 14u(3') are spaced from each other at intervals of one wavelength from each other and are interleaved at one-half wavelength intervals from slots 14u(3), 14u(1) and 14u(2'). In addition, slots 14u(1) and 14u(1') are equally spaced (measured along the YAW AXIS, not numbered) from the axis 14u; slots 14u(2) and 14u(2') are also similarly spaced;
and finally slots 14u(3) and 14u(3') are also similarly spaced.
It will now be recognized that the slots 14u(1) through 14u(3') constitute a linear array with amplitude taper along the PITCH
AXIS, with the centerline of the beam produced by such array broadslde to the waveguide 14u (meaning orthogonal to the plane defined by the PITCH AXIS and the YAW AXIS). Further, the first sidelobe (measured along the axis 14u) is determined in accord-ance with the selected amplitude taper.
Waveguide 12u here is dimensioned so that its width is less than the width of waveguide 14u. Therefore, the wavelength of energy in waveguide 12u is greater than that in waveguide 14u.
In consequence, then, the spacing (measured along axis 12u) between the various slots 12u(1), 12u(2), 12u(1'), 12u(2') is greater than the spacing of the correspondi.ng slots in wavegui.de 14u. It should be noted here that if energy is fed to the same end of waveguide 12u as waveguide 14u, the electrical short circuit (not shown) in the former would be disposed one-quarter wavelength from slot 12u(2') so the sense of the electric field at each pair of corresponding slots in the two waveguides would ; 30 be appropriate along the YAW AXIS.

~147851 The spacing (measured along the YAW AXIS) of each one of the slots 12u(1), 12u(2), 12u(1'), 12u(2') is determined to allow an amplitude taper along the YAW AXIS (without affecting polarization). Therefore, each slot in waveguide 12u is at a greater distance from the axis 12u' than the distance of the corresponding slot in waveguide 14u from the axis 14u'.
Waveguide lOu is dimensioned so that at least two slots lOu(l), lOu(l') may be fitted in the zone defined by the free side of waveguide 12u and the line defining the largest allow-able aperture 11. Here the width of waveguide lOu is .740 inches.
As would be expected, because the wavelength of energy within the waveguide lOu is greater than the wavelength within wave-guide 14u or 12u, slots lOu(l) and lOu(l') are further apart than slots 12u(1) and 12u(1') or 14u(1) and 14u(1'). Also, the position of the electrical short circuit (not shown) near slot lOu(l') is determined b~ the wavelength of the energy in the waveguide lOu and the senses of the electric fields at slots lOu(l) and lOu(l') are, respectively, the same as the senses of the electric fields at slots 14u(1) and 14u(1').
In order to provide a desired amplitude taper along the YAW AXIS, the amount of energy fed into each one of the wave-guides 14u, 12u, lOu, 141, 121, 101 is adjusted in any con-venient manner in the corporate feed (not shown). In addition, the positions (measured along the YAW AXIS) of slots lOu(l), lOu(l') are changed to contribute to the desired amplitude taper so that the shape of the beam along the YAW AXIS is optimized and sidelobes are reduced to a minimum.
It will now be evident to one of skill in the art that, for a slot antenna with a small (meaning in the order of 5"

diameter) circular aperture when designed for X-band, the ~7~35~

flexibility in design offered by using waveguides of different widths is advantageous. That is to say, because the relative positions of corresponding slots in the different waveguides may be adjusted without changing the orientations of such slotsr antenna gain may be maximized for a pencil beam with relatively small sidelobes and without affecting the polariza-tion of such beam. In this connection, it should be noted that the length of each slot also may be adjusted to modify the phase distribution across the aperture. With an a priori knowledge of the effect of changing the len~th of a resonant slot, conventional empirical techniques may be followed to adjust the phase distribution across the aperture for any particular case. Thus, as here where the width of the beam measured along the yaw axis is to be the same as the width of the beam along the pitch axis, the lengths of the slots may be changed to optimize the phase distri.buti.ons along such axes.
It is felt, therefore, that this invention should not be restricted to its disclosed embodiment, but rather should be imited only by the spirit and scope of the appended claims.

Claims (2)

  1. What is claimed is:

    l. A linearly polarized slot array antenna having a substan-tially circular aperture, the ratio between the diameter of such aperture and the wavelength of radio frequency energy at the design frequency of such antenna being in the order of 5:1, such antenna comprising:
    (a) a first plurality of rectangular waveguide resonators dimensioned, when juxtaposed with narrow walls abutting, substantially to cover a first half of the circular aperture, the width of the broad wall of each successive one of such waveguide resonators decreasing outwardly from the centrally located one of such waveguides;
    (b) a second like plurality of rectangular waveguide resonators covering the second half of the circular aperture; and (c) a plurality of radiating slots formed through the broad wall of each one of the rectangular waveguide resonators, such slots being parallel one to another with the center of each different slot lying in a plane of maximum electric field within its corres-ponding rectangular waveguide resonator, the distances of such slots in each such resonator from the center-line thereof increasing from the center to each end of such resonator to provide amplitude taper along the length of such resonators.
  2. 2. The linearly polarized slot array antenna as in claim 1 wherein the distances from the longitudinal axis of successive rectangular waveguide resonators to centers of corresponding slots increases to provide amplitude taper along a line orthogonal to the lengths of such resonators.
CA000361419A 1979-11-26 1980-10-01 Slot array antenna with amplitude taper across a small circular aperture Expired CA1147851A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US9724679A 1979-11-26 1979-11-26
US097,246 1979-11-26

Publications (1)

Publication Number Publication Date
CA1147851A true CA1147851A (en) 1983-06-07

Family

ID=22262432

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000361419A Expired CA1147851A (en) 1979-11-26 1980-10-01 Slot array antenna with amplitude taper across a small circular aperture

Country Status (5)

Country Link
JP (1) JPS5687902A (en)
CA (1) CA1147851A (en)
DE (1) DE3044532A1 (en)
FR (1) FR2470457A1 (en)
GB (1) GB2064876B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59139707A (en) * 1983-01-31 1984-08-10 Mitsubishi Electric Corp Waveguide slot array antenna
JPS59126702U (en) * 1983-02-15 1984-08-25 金井 宏之 automotive wheels
DE4105764A1 (en) * 1991-02-23 1992-08-27 Standard Elektrik Lorenz Ag DEVICE FOR SHAPING AN ANTENNA DIAGRAM IN A SEMICONDUCTOR SLOT ARRAY ANTENNA WITH SERIAL POWER
JP5173810B2 (en) * 2006-08-11 2013-04-03 古野電気株式会社 Slot array antenna
JP6269217B2 (en) * 2014-03-19 2018-01-31 住友電気工業株式会社 Slot antenna and slot antenna device

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2659005A (en) * 1951-03-21 1953-11-10 Ca Nat Research Council Microwave antenna
GB869812A (en) * 1956-11-27 1961-06-07 Emi Ltd Improvements relating to slotted waveguide aerials
US3363253A (en) * 1965-01-18 1968-01-09 Ryan Aeronautical Co Multi-beam resonant planar slot array antenna
US3711858A (en) * 1971-02-24 1973-01-16 Westinghouse Electric Corp Monopulse radar antenna structure
US4121220A (en) * 1975-01-31 1978-10-17 Electronique Marcel Dassault Flat radar antenna employing circular array of slotted waveguides
FR2335064A1 (en) * 1975-12-09 1977-07-08 Dassault Electronique RADAR FLAT ANTENNA
US4038742A (en) * 1976-09-15 1977-08-02 The United States Of America As Represented By The Secretary Of The Army Method of making styrofoam slotted plane-array antenna

Also Published As

Publication number Publication date
FR2470457B1 (en) 1985-03-22
GB2064876A (en) 1981-06-17
DE3044532C2 (en) 1993-04-22
FR2470457A1 (en) 1981-05-29
GB2064876B (en) 1983-11-09
JPS625537B2 (en) 1987-02-05
DE3044532A1 (en) 1981-08-27
JPS5687902A (en) 1981-07-17

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