GB1280841A - Feed system - Google Patents

Feed system

Info

Publication number
GB1280841A
GB1280841A GB40621/69A GB4062169A GB1280841A GB 1280841 A GB1280841 A GB 1280841A GB 40621/69 A GB40621/69 A GB 40621/69A GB 4062169 A GB4062169 A GB 4062169A GB 1280841 A GB1280841 A GB 1280841A
Authority
GB
United Kingdom
Prior art keywords
port
mode
ports
coupled
signals
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
GB40621/69A
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.)
RCA Corp
Original Assignee
RCA Corp
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 RCA Corp filed Critical RCA Corp
Priority to GB134272A priority Critical patent/GB1280842A/en
Publication of GB1280841A publication Critical patent/GB1280841A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/04Multimode antennas
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/06Systems determining position data of a target
    • G01S13/42Simultaneous measurement of distance and other co-ordinates
    • G01S13/44Monopulse radar, i.e. simultaneous lobing
    • G01S13/4409HF sub-systems particularly adapted therefor, e.g. circuits for signal combination
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/02Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
    • G01S3/14Systems for determining direction or deviation from predetermined direction
    • G01S3/146Systems for determining direction or deviation from predetermined direction by comparing linear polarisation components

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Waveguide Aerials (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Waveguide Switches, Polarizers, And Phase Shifters (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

1280841 Aerials; radio direction-finding RCA CORPORATION 14 Aug 1969 [21 Aug 1968] 40621/69 Headings H4A and H4D [Also in Division H1] In a monopulse multimode feed system a first plurality of waveguide modes is provided by first means coupled to a sum mode port of a mode coupler 16, Fig. 1, and a second plurality of waveguide modes is provided by second means coupled to a plurality of difference mode ports of said coupler, the modes of said second plurality being circularly polarized. Third means, including a single aperture radiating horn 18, is coupled to another port of said coupler. As described, the mode coupler 16, Fig. 2 (an end view), has a large conically shaped port 25 at the centre of a square waveguide section and includes eight symmetrically located waveguide ports 26 to 33 in corner pairs forming four circularly polarized exciting sub-apertures, with each port being orthogonally polarized with respect to its corner paired port. The centre port 25 increases in diameter from its end 34 near the receiver equipment to its end 35 near the horn 18. There is a step between the larger end of the port 25 and the square waveguide section for exciting modes higher than the fundamental. Propagation of unwanted modes is prevented by an inner ring 37 in the port 25 and by tuning stubs 40 in the ports 26 to 33. The horn 18 has an increased flare angle at its end and is provided with internal fins along its four sides, and square waveguide sections inside its corners, to improve bandwidth (Fig. 7, not shown). A mode filter 17, in series between the horn 18 and the mode coupler 16, has a square cross-section, a half cosine function profile along the axis of propagation, and symmetrically located ridges in its two main planes (Figs. 5, 6, not shown). The minimum width of the square aperture at the larger end of the mode filter, and the length of said mode filter are, respectively, 2# and 5#, where #=wavelength corresponding to the geometrical mean of the limits of the operating frequency band. Operation in tracking mode.-The total step aperture 36 of the mode coupler 16 is considered as divided into four sub-apertures as shown in Fig. 4, each sub-aperture having a respective horizontally polarized port and a respective vertically polarized port. The ports are coupled in associated pairs 26, 27; 28, 29; 30, 31; 32, 33 to the inputs of respective short slot hybrids 44 to 47. With right-hand circularly ploarized signals, output ports 1, 3, 5, 7 of the hybrids 44 to 47 are coupled to terminations 55 to 58. Output ports 2, 4 of the hybrids 44, 45 are coupled through a waveguide section 48 to the input ports of a hybrid 50, and output ports 6, 8 of the hybrids 46, 47 are coupled through a waveguide section 49 to the input ports of a hybrid 53. Magic tees 52, 53 are each coupled to each hybrid 52, 53 and respectively provide elevation and azimuth difference mode signals at their output ports 61, 62. For left-hand circularly polarized signals, the ports 2, 4, 6, 8 of the hybrids 44 to 47 are terminated, and the ports 1, 3, 5, 7 are used, in conjunction with waveguide sections 59, 60. Also, the roles of the output ports 61, 62 are reversed. Operation with sum mode signals.-These signals are coupled between one port of a threeport polarizer assembly 12, Fig. 1, and the smaller end of the conical port of the mode coupler 16. The assembly 12 includes an orthogonal coupler 71 (Fig. 8, not shown) constructed of square waveguide sections, in which transmitted signals in the TE 10 mode are combined with received signals in the TE 01 mode. A fixed phase shifter 73, in the form of a square waveguide section which is internally ridged and which is provided with two sets of corner irises, converts the orthogonally polarized transmitted and received waves into right- and left-hand circularly polarized waves (Figs. 9, 10, not shown). A rotatable phase shifter 75, which is similar to the fixed phase shifter 73, is provided at each end with a rotary joint 74, 76 and is geared to an electric motor (Fig. 11, not shown). Circularly polarized waves from the fixed phase shifter 73 are accepted by the rotatable assembly and are transformed back to linear polarized waves at the output of the rotary joint 76. The attitude of the output polarizations is dependent upon the orientation of the phase shifter 75, the orthogonal relationship of the transmitted and received waves remaining at all attitudes. By removing the second phase shifter 75 and the rotary joints 74, 76, operation with circularly polarized signals at the horn is obtained. Reference is made to Specification 1,280,842.
GB40621/69A 1968-08-21 1969-08-14 Feed system Expired GB1280841A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB134272A GB1280842A (en) 1968-08-21 1969-08-14 Polarization rotator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US75437368A 1968-08-21 1968-08-21

Publications (1)

Publication Number Publication Date
GB1280841A true GB1280841A (en) 1972-07-05

Family

ID=25034510

Family Applications (1)

Application Number Title Priority Date Filing Date
GB40621/69A Expired GB1280841A (en) 1968-08-21 1969-08-14 Feed system

Country Status (4)

Country Link
US (1) US3560976A (en)
JP (1) JPS5012717B1 (en)
DE (1) DE1942678C3 (en)
GB (1) GB1280841A (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3696434A (en) * 1971-01-15 1972-10-03 Radiation Inc Independent mode antenna feed system
DE2940928A1 (en) * 1978-10-11 1980-04-24 Prl Soc STORAGE HEATER
FR2507826A1 (en) * 1981-06-11 1982-12-17 Thomson Csf PRIMARY SOURCE WITH REUSE OF FREQUENCIES
EP0121612A1 (en) * 1983-04-01 1984-10-17 ATELIERS DE CONSTRUCTIONS ELECTRIQUES DE CHARLEROI (ACEC) Société Anonyme Storage heater equipped with a device for controlling the speed of a fan
DE3381303D1 (en) * 1983-06-18 1990-04-12 Ant Nachrichtentech FOUR-TORCH NETWORK FOR MICROWAVE ANTENNAS WITH MONOPULUS TRACKING.
US4864315A (en) * 1985-11-05 1989-09-05 Itt Avionics Phased array antenna testing arrangement
US4712110A (en) * 1985-12-26 1987-12-08 General Dynamics, Pomona Division Five-port monopulse antenna feed structure with one dedicated transmit port
US4885593A (en) * 1986-09-18 1989-12-05 Scientific-Atlanta, Inc. Feeds for compact ranges
US5175555A (en) * 1991-03-15 1992-12-29 Harris Corporation Combined radar altimeter, radiometer sensor employing multiport feed horn having blended sidewall geometry
US5329285A (en) * 1991-07-18 1994-07-12 The Boeing Company Dually polarized monopulse feed using an orthogonal polarization coupler in a multimode waveguide
US5870060A (en) * 1996-05-01 1999-02-09 Trw Inc. Feeder link antenna
GB0405112D0 (en) * 2004-03-06 2004-04-07 Univ Belfast Single aperature monopulse antenna
US20100238086A1 (en) * 2009-03-17 2010-09-23 Electronics And Telecommunications Research Institute Double-ridged horn antenna having higher-order mode suppressor
WO2018216210A1 (en) * 2017-05-26 2018-11-29 三菱電機株式会社 Polarization separation circuit
EP4020700A1 (en) * 2020-12-22 2022-06-29 A.D.S. International S.r.l. Antenna and antenna system for satellite communications

Also Published As

Publication number Publication date
DE1942678A1 (en) 1970-05-21
JPS5012717B1 (en) 1975-05-14
DE1942678C3 (en) 1980-09-18
US3560976A (en) 1971-02-02
DE1942678B2 (en) 1979-12-20

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PE20 Patent expired after termination of 20 years