EP0191031A1 - Multibeam antenna, which can provide different beam positions according to the angular sector of interest - Google Patents

Multibeam antenna, which can provide different beam positions according to the angular sector of interest

Info

Publication number
EP0191031A1
EP0191031A1 EP85903361A EP85903361A EP0191031A1 EP 0191031 A1 EP0191031 A1 EP 0191031A1 EP 85903361 A EP85903361 A EP 85903361A EP 85903361 A EP85903361 A EP 85903361A EP 0191031 A1 EP0191031 A1 EP 0191031A1
Authority
EP
European Patent Office
Prior art keywords
sub
multibeam antenna
provide different
antenna
different beam
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.)
Withdrawn
Application number
EP85903361A
Other languages
German (de)
French (fr)
Inventor
Rosario Scarpetta
Pasquale Russo
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.)
Leonardo SpA
Original Assignee
Selenia Industrie Elettroniche Associate SpA
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 Selenia Industrie Elettroniche Associate SpA filed Critical Selenia Industrie Elettroniche Associate SpA
Publication of EP0191031A1 publication Critical patent/EP0191031A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/24Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/26Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system 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

Definitions

  • This invention concerns a multibeam antenna which has a high switching capability with high RF power levels.
  • the invention may find, application in the field of electronic defence systems fay tackling single or multiple threats arriving from different directions.
  • the antenna can provide pseudo adaptability to the radar cross section, as it is made up of three sub arrays, each of which includes eight elementary equispaced radiators which assure angular coverage of the azimuth emispace from 0° to 180°, fed by a single beamshaping network which provides the correct field amplitude and phase distribution.
  • the emispace is therefore divided into-three angular sectors, each of which a sub array is associated. Switching between these angular sectors and within each sector is electronic.
  • Each sub array shapes three beams which take different angular positions on the azimuth plane through the same feed network. The selection of these beams is electronic upon designation by the system which assesses relevant direction of arrival.
  • One of the previous solutions was to utilize arrays fed by Rothman lenses or by Butler matrixes.
  • An other solution was provided by a series of directional antennas, one for each beam to shape, fed by a n way switch (as many ways as the number of beams) or by transmitters.
  • the antenna which is the subject of this invention, consists of three sub arrays (5), (6), (7) which suitably spaced, can assure angular coverage in the 0° : 180° azimuth emispace. ( In a specular manner, three more sub arrays, fed by a separate transmitter, can assure angle coverage in the other 180° : 360° azimuth emispace).
  • the three sub arrays are fed by a single beamforming network which provides for the correct field amplitude & phase distribution to each subarray.
  • the emispace is thus divided into three angle sectors, to each one of which a sub array is associated. Switching between these angular sectors is performed electronically and within each sector; the relevant sub array forms three beams which take different angle directions on the azimuth plane through the same feed network.
  • the beam switching and farming network consists of solid state components to obtain the high switching speeds (100-150 nsec) which are required to satisfy the tasks set on the system.
  • the gain of each beam, required to established the necessary effective radiated power is achieved by providing the array with a directivity also in the vertical plane. This can be achieved by using as an element of the array a sectorial horn radiator, over the aperture of which a phase correcting dielectric lens is placed, which enhances radiation efficiency.
  • a most interesting characteristic of this indicating system is that of directing the beam to the desired direction in negligible times. This is achieved through:
  • the transmitting antenna is made up of two specular subassemblies each covering a 180° sector. It may be installed, in its preferred configuration, on board a ship ( Figure 1).
  • Figure 1 Schematic representation of the system fitted on board a ship.
  • Figure 5 Delay line phase shifter, indicated as a whole with numbers (2) (3) (4) in Figure 3.
  • Figure 6 Piirt circuit, where d stands for the desired direction, 3a, 3c and 4 are the signals which enable each relevant block 3a, 3c and 4. (Figure 2) to deliver RF power in the desired directi ⁇ n.
  • Figure 7 Detail of one of the sub arrays where X, Y, Z are the reference system;
  • (5a) is the radiating element
  • (9) is the dielectric lens for field phase correction over the varying element
  • the antenna systems operation will be described: the input RF signal (1) is split by the power divider (2) into eight parts, which are sent to the delay line phase shifter (3).
  • the delay live phase shifter (3) provides the correct phase illumination to sub array (5) or (6) or (7) to radiate the RF signal in the desired direction.
  • Such phase shifter consists of delay lines (36) either coaxial or triplate to assure stability in the radiation direction over the whole range of frequencies of operation.
  • the switching network (selector) (4) which follows the phase shifter (3) switches the predetermined distribution onto one of the three sub arrays (5), (6), (7) which are geometrically set to achieve the coverage required (0° : 180°).
  • the commands to the delay line phase shifter (3) and to the switching network (sub array selector) (4) are provided in parallel to the pilot circuit (8) as a function of the desired position of the beam.
  • This pilot circuit can select the output signals, corresponding to the input signal, required to drive the beam selectors 3a & 3c and the sub array selector (4) and then to deliver RF power in the desired direction.
  • the insertion loss of the phase shifting splitting & switching network is ⁇ dB so that the antenna gain, inclusive of losses, is 18 dB.
  • the centre subarray ( Figure 3) covers the angular sector from 67.5° to 112.5°, while the two sub arrays (5), (7), cover each0°:67.5° and 112.5°: 180°. This gain distribution may be exploited to make the antenna system pseudoadaptive to ship R.C.S. for a more effective electronic defence (ECM) of the same.
  • ECM electronic defence
  • This adaptation provides the antenna system also with a pseudoadapting capability to the ship radar cross section, as in the angular sector where this is larger, there is a larger array gain and therefore higher effective radiated power, known in leterature as ERP.

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Aerials With Secondary Devices (AREA)

Abstract

Antenne multidirectionnelle possédant une grande capacité de commutation avec des niveaux de puissance HF élevés, se composant de trois sous-rangées (5, 6, 7) lesquelles, espacées de manière appropriée, assurent une couverture angulaire dans l'hémiespace azimutal entre 0o et 180o. Un réseau formant un faisceau unique (2, 3) confère à chaque sous-rangée l'amplitude de champ et la distribution de phase correctes. La commutation est effectuée électroniquement.Multidirectional antenna having high switching capacity with high RF power levels, consisting of three sub-rows (5, 6, 7) which, suitably spaced, provide angular coverage in the azimuthal hemispace between 0o and 180o . A single beam array (2, 3) gives each sub-row the correct field amplitude and phase distribution. The switching is carried out electronically.

Description

"MULTIBEAM ANTENNA, WHICH CAN PROVIDE DIFFERENT BEAM POSITIONS ACCORDING TO THE ANGULAR SECTOR OF INTEREST"
This invention concerns a multibeam antenna which has a high switching capability with high RF power levels.
It belonges to the field of electronically switched beam antennas. The invention may find, application in the field of electronic defence systems fay tackling single or multiple threats arriving from different directions. The antenna can provide pseudo adaptability to the radar cross section, as it is made up of three sub arrays, each of which includes eight elementary equispaced radiators which assure angular coverage of the azimuth emispace from 0° to 180°, fed by a single beamshaping network which provides the correct field amplitude and phase distribution.
The emispace is therefore divided into-three angular sectors, each of which a sub array is associated. Switching between these angular sectors and within each sector is electronic. Each sub array, as mentioned above, shapes three beams which take different angular positions on the azimuth plane through the same feed network. The selection of these beams is electronic upon designation by the system which assesses relevant direction of arrival. One of the previous solutions was to utilize arrays fed by Rothman lenses or by Butler matrixes. An other solution was provided by a series of directional antennas, one for each beam to shape, fed by a n way switch (as many ways as the number of beams) or by transmitters. These solutions have a number of drawbacks, among which: - proliferation of the number of transmitters, with consequential cost and dimensions increase; - low- switching speed, for the switching network, due tα the high RF levels at stake. The antenna, which is the subject of this invention, consists of three sub arrays (5), (6), (7) which suitably spaced, can assure angular coverage in the 0° : 180° azimuth emispace. ( In a specular manner, three more sub arrays, fed by a separate transmitter, can assure angle coverage in the other 180° : 360° azimuth emispace). The three sub arrays are fed by a single beamforming network which provides for the correct field amplitude & phase distribution to each subarray. The emispace is thus divided into three angle sectors, to each one of which a sub array is associated. Switching between these angular sectors is performed electronically and within each sector; the relevant sub array forms three beams which take different angle directions on the azimuth plane through the same feed network.
Selection of these beams is in turn electronic, upon indication from the designating system, i.e. the system which descerns the threat or threats direction of arrival. The beam switching and farming network consists of solid state components to obtain the high switching speeds (100-150 nsec) which are required to satisfy the tasks set on the system. The gain of each beam, required to established the necessary effective radiated power, is achieved by providing the array with a directivity also in the vertical plane. This can be achieved by using as an element of the array a sectorial horn radiator, over the aperture of which a phase correcting dielectric lens is placed, which enhances radiation efficiency. A most interesting characteristic of this indicating system is that of directing the beam to the desired direction in negligible times. This is achieved through:
- high switching times with high total RF power radiated;
- high effective radiated power associated to each single beam;
- azimuth coverage over the whole round angle using two radiating systems, each having a 0° to 180° coverage sector;
- capability to adapt to the number of beams of the designating system. This gives the antenna system the capability to tackle multiple threats.
The transmitting antenna is made up of two specular subassemblies each covering a 180° sector. It may be installed, in its preferred configuration, on board a ship (Figure 1).
The invention will now be described with reference to one of its forms presently preferred and provided as an illustration, but not limited to such form, with reference to figures and diagrams attached. Figure 1 : Schematic representation of the system fitted on board a ship.
Figure 2: Functional schematic of the antenna, consisting
- Transmitter (1)
- Power divider (2) - Delay line phase shifter (3) where 3a and 3c are beam selectors and 3b are the delay lines
- Sub array selector (4)
- Three sub arrays (5) (6) (7)
- Pilot circuit (8) Figure 3: Block diagram of the antenna system where:
(4) switching network (sub array selector); (3) delay line phase shifter;
(2) power splitter;
(5) (6) (7) sub arrays; Figure 4r Power splitter (noted as (2) in Figure 3). Here numbers 1 to 8 indicate the RF signal outputs and IN is the input signal.
Figure 5: Delay line phase shifter, indicated as a whole with numbers (2) (3) (4) in Figure 3. Figure 6: Piirt circuit, where d stands for the desired direction, 3a, 3c and 4 are the signals which enable each relevant block 3a, 3c and 4. (Figure 2) to deliver RF power in the desired directiσn. Figure 7: Detail of one of the sub arrays where X, Y, Z are the reference system;
(5a) is the radiating element;
(9) is the dielectric lens for field phase correction over the varying element;
(10) is the polarization converter. Figure 8: Correspondence between the three sub arrays angular coverage and the designating system's angular coverage. With reference to the figures, the antenna systems operation will be described: the input RF signal (1) is split by the power divider (2) into eight parts, which are sent to the delay line phase shifter (3). The delay live phase shifter (3) provides the correct phase illumination to sub array (5) or (6) or (7) to radiate the RF signal in the desired direction. Such phase shifter consists of delay lines (36) either coaxial or triplate to assure stability in the radiation direction over the whole range of frequencies of operation.
The switching network (selector) (4) which follows the phase shifter (3) switches the predetermined distribution onto one of the three sub arrays (5), (6), (7) which are geometrically set to achieve the coverage required (0° : 180°). The commands to the delay line phase shifter (3) and to the switching network (sub array selector) (4) are provided in parallel to the pilot circuit (8) as a function of the desired position of the beam.
This pilot circuit can select the output signals, corresponding to the input signal, required to drive the beam selectors 3a & 3c and the sub array selector (4) and then to deliver RF power in the desired direction. The insertion loss of the phase shifting splitting & switching network is δ dB so that the antenna gain, inclusive of losses, is 18 dB. For each subassy, nine beam positions are achieved. The centre subarray (Figure 3) covers the angular sector from 67.5° to 112.5°, while the two sub arrays (5), (7), cover each0°:67.5° and 112.5°: 180°. This gain distribution may be exploited to make the antenna system pseudoadaptive to ship R.C.S. for a more effective electronic defence (ECM) of the same. The uniqueners of this antenna system consists essentially in:
- the use of the array principle to switch large RF powers rapidly over different angular directions (100 : 150 nsec); - the adaptation to the designating system through the use of a single transmitter associated to a single feed network which manages three subarrays to cover the angular emispace.
This adaptation provides the antenna system also with a pseudoadapting capability to the ship radar cross section, as in the angular sector where this is larger, there is a larger array gain and therefore higher effective radiated power, known in leterature as ERP.

Claims

1. Multibeam antenna which can provide different beam positions, where these positions are acquired in very short times, with high RF power, characterized by including arpower splitter (2), a delay line phase shifter (3) a sub array selector (4) and three sub arrays (5), (6), (7).
2. Multibeam antenna, as per claim 1, characterized by furthermore including a pilot circuit (6) which has the task of commanding the delay line phase shifter (3) and the sub array (4) to deliver the RF power in the desired direction.
3. Multibeam antenna, as per claims above, inclusive also of three sub arrays fed by a single splitting, phasing and switching network which provide different angle coverage.
4. Multibeam antenna, as per previous descriptions, drawings and claims above, in its wholeness and single components.
EP85903361A 1984-07-09 1985-07-03 Multibeam antenna, which can provide different beam positions according to the angular sector of interest Withdrawn EP0191031A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT4853484 1984-07-09
IT48534/84A IT1179394B (en) 1984-07-09 1984-07-09 MULTI-BAND ANTENNA ABLE TO REALIZE DIFFERENT BEAM POSITIONS ACCORDING TO THE ANGULAR SECTOR OF INTEREST

Publications (1)

Publication Number Publication Date
EP0191031A1 true EP0191031A1 (en) 1986-08-20

Family

ID=11267149

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85903361A Withdrawn EP0191031A1 (en) 1984-07-09 1985-07-03 Multibeam antenna, which can provide different beam positions according to the angular sector of interest

Country Status (3)

Country Link
EP (1) EP0191031A1 (en)
IT (1) IT1179394B (en)
WO (1) WO1986000760A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2734410B1 (en) * 1986-08-05 1997-07-25 Thomson Csf Radant MICROWAVE ANTENNA WITH RADIATION DIAGRAM SYNTHESIS
US4766438A (en) * 1987-02-27 1988-08-23 Hughes Aircraft Company Three dimensional feed through lens with hemispherical coverage
JPS6478177A (en) * 1987-09-21 1989-03-23 Nec Corp Landing guiding device
JPH06105959B2 (en) * 1989-04-24 1994-12-21 三菱電機株式会社 Electronic scanning array antenna device
US5025493A (en) * 1989-06-02 1991-06-18 Scientific-Atlanta, Inc. Multi-element antenna system and array signal processing method
US4973971A (en) * 1989-12-18 1990-11-27 Allied-Signal Inc. Broadband circular phased array antenna
GB2356096B (en) 1991-03-12 2001-08-15 Siemens Plessey Electronic Method of operating a radar antenna system
US5552798A (en) * 1994-08-23 1996-09-03 Globalstar L.P. Antenna for multipath satellite communication links
DE60032710T2 (en) * 1999-11-03 2007-11-08 Intel Corporation, Santa Clara Router with room multiplex circuit for wireless data packets
DE102014106060A1 (en) * 2014-04-30 2015-11-19 Karlsruher Institut für Technologie antenna array

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3816830A (en) * 1970-11-27 1974-06-11 Hazeltine Corp Cylindrical array antenna
GB1553916A (en) * 1975-06-09 1979-10-10 Commw Scient Ind Res Org Modulation of scanning radio beams
US4124852A (en) * 1977-01-24 1978-11-07 Raytheon Company Phased power switching system for scanning antenna array

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8600760A1 *

Also Published As

Publication number Publication date
IT1179394B (en) 1987-09-16
IT8448534A0 (en) 1984-07-09
WO1986000760A1 (en) 1986-01-30

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