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Publication numberUS3157878 A
Publication typeGrant
Publication dateNov 17, 1964
Filing dateSep 26, 1960
Priority dateSep 26, 1960
Publication numberUS 3157878 A, US 3157878A, US-A-3157878, US3157878 A, US3157878A
InventorsHansel Paul G, Paulstich William H, Richter Frederick G
Original AssigneeServo Corp Of America
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Broadband antenna array
US 3157878 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)


signors to Servo Corporation of America, Hiclisvilie, N.Y., a corporation at New York Filed Sept. 26, N60, Ser. No. 58,429 4 Claims. (6i. 343- 1l3) This invention relates to direction finding antennas and, more particularly, to a broadband antenna array for utilization in quasi-Doppler direction finding equipment.

A Doppler direction finding system generally employs a rotating antenna, as contrasted to a quasi-Doppler direction finding system which utilizes a plurality of antenna elements fixed in a predetermined array to simulate the effects of revolving a single receiving antenna around a circle. This is accomplished by commutation of a large number of fixed elements in such a manner, that only one or at most two elements are active at any one instant. The remaining momentarily inactive elements should be as non-receptive to the incoming radiation as possible.

In the operation of conventional direction finders, the system accuracy and sensitivity is severely affected if oper ation is attempted through the antenna resonance frequency, because the inactive elements act as parasitic reradiators causing a material alteration in the received field configuration from that which is postulated for successful operation of the direction finder. Consequently, in the operation of such systems, parasitic reradiation has been avoided by utilizing antenna configurations that are resonant above the highest frequency encountered in operation. However, by using this type of configuration a material reduction in the utility of the direction finder is suffered because the configuration is ineficient at some frequency levels in a broad band of operation.

Accordingly, it is an object of the invention to provide an antenna array for a quasi-Doppler direction finding system which is operable with accuracy and sensitivity in a broad frequency range including antenna resonant fre quencies.

Another object of the invention is to provide a direction finding antenna array in which parasitic reradiation is suppressed in the inactive antenna elements whereby the operable frequency range of the array is broadened.

A further object is to provide a dynamic impedance arrangement in a direction finding antenna array for suppressing parasitic reradiation of energy from the inactive antenna elements.

In accordance with an aspect of the invention, there is provided a circular array of antenna elements. Each of the elements includes a plurality of antenna segments and impedance elements for coupling each adjacent pair of segments. Commutating means are provided for coupling in succession a communication system to the antenna elements. The invention is characterized by means for reducing or substantially eliminating the impedance between segments of only the antenna coupled to the communication system, whereby parasitic reradiation by the idle antenna elements is substantially suppressed.

The above mentioned and other features and objects of this invention and the manner of attaining them will 1 become more apparent and the invention itself will be best understood by reference to the following description of an embodiment of the invention taken in conjunction With the accompanying drawing, wherein:

FIG. 1 is a schematic diagram of an antenna array and communication system; and

FIG. 2 is a schematic diagram of an antenna element of an array and the commutating and control circuitry for it. a

Referring now to FIG. 1, a plurality of antenna ele- 3,157,878 Patented Nov; 17, 1954 "ice ments 1145 are arranged in a circular or other suitably configurated array to form a conventional quasi-Doppler antenna. Antenna impedance control circuits l1al5a and commutator contacts lib-15b are connected to the elements 1145, respectively. Each control circuit la-15a is also provided with a commutator contact 150, respectively. In practice, the impedance control circuit and contacts (which are suggested only by way of example) are closely located with the other electronic understood that they maybe any suitable type of wiper arm or electronic switch for use with an appropriate cornmutator assembly.

Each antenna element 1l15, for example, element 13 (FIG. 2) comprises a plurality of segments 1911-15 which are preferably arranged as a folded dipole by coupling each adjacent pair of segments together by a dynamic impedance, such as diodes Ztla-Zlll. Thecoupling diodes are connected to conduct from a common terminal 21 through the opposite dipole branches of the antenna element to ground. A connection 13b extends from the common terminal 21 for intermittent contact with the commutator wiper arm. I

The dynamic impedance elements, While described as being conventional diodes Zita-2W, may also be inductive or capacitive elements, such as voltage sensitive barium titanate capacitors or capacity diodes. It is only essential that the impedance elements utilized to couple the antenna segments vary in impedance from substantially a short-circuit condition to substantially an open-circuited condition, dependent on the control voltages that are applied. When an antenna element is inactive, the impedance elements are open-circuited by the impedances to effectively segment the antenna element and thereby practically eliminate any parasitic reradiation from this element. However, when an antenna element is activated, the impedance elements are short-circuited to remove the loading from the antenna; i.e. substantially to return the antenna to a condition free of interposed impedances.

By way of illustration, the antenna control circuit 13a, which provides the voltages for controlling the operating condition of the impedance elements, may comprise a source of energy, such as a battery 22, and a conventional double armature relay 23. Each relay armature 24-25 operates as a switch with a pair of fixed contacts 26-27, iii-2 respectively. The contacts 26-27 are connected to the positive and negative terminals, respectively, of the battery 22. The contact 28 is connected to the terminal 21 of the antenna element by the line 3%, while the contact 29 is multipled to the anode terminal ALAIZ of each of the diodes 2fia2tll, respectively.

The energizing coil 31 for relay 23 is connected to ground at one end and to commutator contact at the other end. Under normal conditions, the relay winding 31 is not energized and the armatures 2425 are in contact with the contacts 27 and 29, respectively, to complete the circuit from the negative terminal of the battery 22 through the armatures to the anode elements of each of the diodes Zita-2th, so that these diodes are non-conductive.

However, as the commutator assembly 18 sweeps a circular path, the contacts 13b and 130, are brushed by the assembly 18 to activate the antenna element by commutation with the communication system 17. When this occurs, the relay winding 31 is energized by a pulse from the commutation generator 16 to attract armatures 24-25 to the contacts 2628, respectively. In this position, voltage of positivepolarity is coupled over line 30 to the common terminal 21 of the antenna element. The application of positive voltage to the antenna element renders the diodes 20a-20'l conducting thereby effectively removing the impedance loading of the antenna element, and permitting it to receive radiant energy from a remote source (not shown).

While the communication system is coupled to one antenna element, the remaining elements are inactive. During this period, the relay armatures 24 25 of the antenna control circuit are in a normal position, that is, in contact with contacts 27-29 coupling energy of negative polarity to each of the diode anodes. The diodes are back-biased by the applied voltage thereby rendering them non-conductive. When the diodes are non-conducting their impedance is practically infinite, thereby efiectively 'loading the antenna element into non-radiating segments; thus, the flow of current in the antenna is insignificant and parasitic reradiation is effectively suppressed.

Since *the parasitic reradiation of energy from momentarily inactive antenna elements is suppressed, the sensitivity of 'a direction finding system, utilizing this type of antenna arrangement, is materially increased. Furthermore, the frequency range may be. extended, permitting operation through resonant frequencies.

While the foregoing description sets forth the principles of the invention in connection with specific apparatus, it is to'be understood that this description is made only by wayof example and not as a limitation of the scope of the'invention as set forth in the objects thereof and in the accompanying claims. -For example, while the sys *tem'has been described in conjunction with the reception ofenergy by a communications system coupled to a direction finding antenna array, it is to be understood that the-invention is equally applicable to a transmitting antenna array where a signal source is sequentially coupled to each of a plurality of circumferentially disposed antenna elements.

What is claimed is:

1. In combination, an antenna array comprising a plurality of antenna elements, a communication system,

commutating means coupled to said communication sys-v namic impedances in an antenna element while said ele-.

ment is coupled to said communication system.

2. The combination according to claim 1, wherein said dynamic impedance means comprises a plurality of unidirectional conducting devices, each device coupling an adjacent pair of segments, and said devices being responsive to the impedance reducing means to conduct While said element is coupled to said communication system.

3. The combination according to claim 2, and also comprising means for normally biasing each of said devices to prevent conduction thereof and suppress parasitic reradiation from the inactive antenna elements.

4. The combination according to claim ,3, wherein said antenna array comprises a quasi-Doppler direction, finding array for receiving directional signals at said communication system.

References Cited inthe file of this patent UNlTED STATES PATENTS 2,210,666 Herzog Aug. 6, 1940 2,466,354 Bagnall Apr. 5, 1949 2,693,583 Rigrod Nov. 2, .1954

FOREIGN PATENTS 678,290 Germany July 12, 1939 1,043,424 Germany Nov. 13, .1958

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2210666 *Jan 9, 1937Aug 6, 1940Lorenz C AgHigh frequency radiation structure
US2466354 *Jun 28, 1944Apr 5, 1949American Telephone & TelegraphDirectional radio system
US2693583 *Aug 29, 1951Nov 2, 1954Westinghouse Electric CorpElectronic cutoff switch
DE678290C *Aug 28, 1935Jul 12, 1939Telefunken GmbhAnordnung zur Tastung zweier Antennengebilde im Rhythmus komplementaerer Zeichen
DE1043424B *Nov 8, 1957Nov 13, 1958Telefunken GmbhRichtantenne mit schwenkbarem Diagramm
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3396394 *Sep 15, 1965Aug 6, 1968Rca CorpDirective antennas
US4005432 *Nov 11, 1975Jan 25, 1977Rockwell International CorporationCommutated log periodic antenna array for automatic direction finding
US4551727 *Dec 23, 1982Nov 5, 1985Cunningham David CRadio direction finding system
US5434575 *Jan 28, 1994Jul 18, 1995California Microwave, Inc.Phased array antenna system using polarization phase shifting
U.S. Classification342/418, 343/876, 342/403
International ClassificationG01S3/54, G01S3/14
Cooperative ClassificationG01S3/54
European ClassificationG01S3/54