US2925595A - Monopulse transmitting and receiving systems - Google Patents
Monopulse transmitting and receiving systems Download PDFInfo
- Publication number
- US2925595A US2925595A US609151A US60915156A US2925595A US 2925595 A US2925595 A US 2925595A US 609151 A US609151 A US 609151A US 60915156 A US60915156 A US 60915156A US 2925595 A US2925595 A US 2925595A
- Authority
- US
- United States
- Prior art keywords
- transmitting
- monopulse
- guides
- radiators
- receiving
- 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 - Lifetime
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S13/00—Systems 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
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/42—Simultaneous measurement of distance and other co-ordinates
- G01S13/44—Monopulse radar, i.e. simultaneous lobing
- G01S13/4409—HF sub-systems particularly adapted therefor, e.g. circuits for signal combination
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q13/00—Waveguide horns or mouths; Slot antennas; Leaky-waveguide antennas; Equivalent structures causing radiation along the transmission path of a guided wave
- H01Q13/06—Waveguide mouths
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q25/00—Antennas or antenna systems providing at least two radiating patterns
- H01Q25/02—Antennas or antenna systems providing at least two radiating patterns providing sum and difference patterns
Definitions
- the present invention relates to aerials for monopulse type radars.
- the antenna in radars of this type, must have a transmitting radiation pattern comprising a single directive lobe, and a receiving pat-tern having four directive lobes intersecting each other, preferably at a level of about 3 db below the level corresponding to the maximum radiation.
- the receiving antenna generally comprises a paraboloid illuminated by four horns.
- the transmitting aerial of the simplest type consists of an additional horn located at the center of a square at the apices of which the four receiving horns are respectively located, However, on account of the required increase in size, such an arrangement is unpractical. It should, furthenbe noted, that the minimum spacing which it is necessary to provide between the four receiving horns, prevents-the receiving patterns from intersecting at the desired 3 vdb level.”
- the device according to the invention comprises a reflector illuminated from four different radiators provided with a correcting device for bringing closer to one another their respective phase centers, means for feeding in phase the ultra high frequency pulse energy to said four radiators to combine their respective radiation patterns into a single directive lobe, and, switch means, to make these radiators independent of one another when operating as receiving elements, to provide four individual radiating patterns.
- the four radiators are four wave-guides placed side by side. These four guides are terminated by resonant windows and the arrangement is completed by a correcting device comprising four inwardly converging flanges, which brings the respective phase centers of the four guides closer to one another. Matching means are preferably provided in the guides, and the windows are uncoupled from each other in any conventional manner.
- Fig. 1 is a diagrammatic view of an end cross-section of the four wave guide radiator used in the device of the invention
- Fig. 2 is the same cross-section, showing the four resonant windows
- Fig. 3 is a perspective view of the wave guides of Fi 2;
- Figs. 4A and 4B are respectively a plan and an elevated view of the svstem of Fig. 3;
- Fig. 5 is a diagrammatic plan view of an embodiment of the invention.
- Fig. 6 shows diagrammatically a system according to the invention
- Fig. 7 is a view of a particular embodiment of the device, by way of example.
- Figs. 8, 9 and 10 are the radiation patterns of a system according to the invention.
- Fig. 1 shows four open wave-guides 1,2,3 and 4 placed side'by side, and having phase centers (p (p ga n
- the level at which the lobes respectively radiated by the tour guides, intersect is found'to be at least 10 db below the maximum "level. If,'a paraboloid of greater focal distance is used to decrease this level to about 3 db, the guides which, in this case, are located at a great distance from the paraboloid, would radiate outwardly with respect to the latter.
- the level is readily brought to 3 db.
- the four guides 1, 2, 3 and 4 are closed respectively by means of resonant windows 5, 6, 7 and 8.
- the distances between the centers of these windows are selected in such a manner that the axis of the four corresponding radiation beams, lie, two by two, in rectangular planes, symmetrically with respect to the focal axis of the paraboloid.
- a correcting device is placed in front of this arrange ment.
- This device comprises convergent flangesll', 12,
- Fig. 5 shows diagrammatically and in cross-section the transmitting and receiving device of the invention. It comprises a parabolic reflector 15 and feeding guides 51, 54 and 52,53.
- This switching arrangement enables the system to pass from the transmitting position, the four guides being fed in phase, to the receiving position, where each of the guides operates independently of one another.
- the switching is provided, according to the invention, by jllIlClllOllS, T.R. and A.T.R. switches disposed as shown in Fig. 6.
- Four magic tees 55 to 58 are disposed between the radiating elements 1 to 4 and the energy source 69.
- the energy supplied by source 69 is divided into two equal fractions by tee 55 each of these fractions being again divided into two. further equal fractionsby means of tees 56 and 57.
- Each of the radiators thus receives substantially a quarter of the available energy, and the radiators are fed in-phase if the lengths of the guides connecting the 7 2,925,595 7 Patented Feb, 16,
- a receiver 72 connected to guide 68, the latter being coupled to guide 67 by duplexer 71, of a conventional type.
- the difference (1+2)-(3+4) formed in arm 60 provides, as is well known, the error voltage corresponding to the angle of elevation of the target. This voltage is then used in a second receiver 73, connected to the vertical arm of tee 55 by means of T.R. device 63.
- FIG. 7 shows a practical embodiment of the invention, wherein same reference numbers have been used to designate same elements as in the preceding figures.
- Curves shown in Figs. 8, 9 and 10, illustrate the results obtained during tests, with a frequency of 9,375 megacycles. This axis of the radiated beam is directed along the axis of the paraboloid reflector.
- the aperture angle of the transmission beam, measured at a level of 3 db is 2 4' and at 10 db is less than 5.
- the four reception patterns intersect at a level of about 3 db.
- the aperture angles at 3 db and at 10 db were respectively 2 3 and less than 5.
- a transmitting and receiving device of the monopulse type comprising: a reflector; and a first, a second, a third and a fourth rectangular radiator disposed side by side and having respectively, a first, a second, a third, and a fourth phase centers, said phase centers being located respectively at the four apices of a rectangle; said first, second, third and fourth radiators having respectively a first, a second, a third and a fourth resonant window directed towards said reflector, the respective distances between the centers of said windows being respectively smaller than the respective distances of said phase centers; the outer edges of said radiators thus forming a rectangle, and two pairs of flanges having outer edges converging by pairs, directed towards said reflector and forming the lateral walls of a truncated pyramid whose large base contacts said rectangle formed by said outer edges of said radiators and whose small base is defined by said outer edges of said flanges; and means for feeding in phase to said radiators the ultra high frequency pulse modulated energy to be transmitted, and
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aerials With Secondary Devices (AREA)
- Radar Systems Or Details Thereof (AREA)
Description
Feb. 16, 1960 L. THOUREL 2,925,595
MONOPULSE TRANSMITTING AND RECEIVING SYSTEMS Filed Sept. 11, 1956 3 Sheets-Sheet 1 )3 x yx THOUREL 2,925,595
MONOPULSE TRANSMITTING AND RECEIVING SYSTEMS Feb. 16, 1960 5 Sheets-Sheet 2 Filed Sept. 11, 1956 LOAD g-mw RECEIVER DUPL [XE R Feb. 16, 1960 2,925,595
MONOPULSE TRANSMITTING AND RECEIVING SYSTEMS Filed Sept. 11, 1956 L. THOUREL 3 Sheets-Sheet 3 MONOPULSE TRANSMITTING AND RECEIVING SYSTEMS Leo Thonrel, Paris, France, assignor to Compagnie Generale de Telegraphic Sans Fil, a corporation of France Application September 11, 1956, Serial No. 609,151
Claims priority, application France September 21, 1955 1 Claim. (Cl. 343-46) The present invention relates to aerials for monopulse type radars.
It is known that, in radars of this type, the antenna must have a transmitting radiation pattern comprising a single directive lobe, and a receiving pat-tern having four directive lobes intersecting each other, preferably at a level of about 3 db below the level corresponding to the maximum radiation.
The receiving antenna generally comprises a paraboloid illuminated by four horns. The transmitting aerial of the simplest type consists of an additional horn located at the center of a square at the apices of which the four receiving horns are respectively located, However, on account of the required increase in size, such an arrangement is unpractical. It should, furthenbe noted, that the minimum spacing which it is necessary to provide between the four receiving horns, prevents-the receiving patterns from intersecting at the desired 3 vdb level." I
It is an object of the present invention to provide a transmitting-receiving device in which these difficulties are avoided. The device according to the invention comprises a reflector illuminated from four different radiators provided with a correcting device for bringing closer to one another their respective phase centers, means for feeding in phase the ultra high frequency pulse energy to said four radiators to combine their respective radiation patterns into a single directive lobe, and, switch means, to make these radiators independent of one another when operating as receiving elements, to provide four individual radiating patterns.
According to a particular embodiment of the invention, the four radiators are four wave-guides placed side by side. These four guides are terminated by resonant windows and the arrangement is completed by a correcting device comprising four inwardly converging flanges, which brings the respective phase centers of the four guides closer to one another. Matching means are preferably provided in the guides, and the windows are uncoupled from each other in any conventional manner.
The construction and operation of the invention will be better understood from the following specification, and the appended drawing, wherein:
Fig. 1 is a diagrammatic view of an end cross-section of the four wave guide radiator used in the device of the invention;
Fig. 2 is the same cross-section, showing the four resonant windows;
Fig. 3 is a perspective view of the wave guides of Fi 2;
Figs. 4A and 4B are respectively a plan and an elevated view of the svstem of Fig. 3;
Fig. 5 is a diagrammatic plan view of an embodiment of the invention;
Fig. 6 shows diagrammatically a system according to the invention;
Fig. 7 is a view of a particular embodiment of the device, by way of example;
Figs. 8, 9 and 10 are the radiation patterns of a system according to the invention;
Fig. 1 shows four open wave- guides 1,2,3 and 4 placed side'by side, and having phase centers (p (p ga n When the mouths of such guides are placed at the focus of a paraboloid of conventional focal distance and size, the level at which the lobes respectively radiated by the tour guides, intersect, is found'to be at least 10 db below the maximum "level. If,'a paraboloid of greater focal distance is used to decrease this level to about 3 db, the guides which, in this case, are located at a great distance from the paraboloid, would radiate outwardly with respect to the latter. If the respective phase centers of the guides 1 through 4 are brought as close to each other as possible by the provision of resonant windows 21, 22, 23 and 24, as shown in Figure 2, this enables the intersection of the radiation patterns to take place at about 6 db, which, however, is still insufiicient.
By means of the invention, the level is readily brought to 3 db.
Referring to Figure 3, the four guides 1, 2, 3 and 4 are closed respectively by means of resonant windows 5, 6, 7 and 8. The distances between the centers of these windows are selected in such a manner that the axis of the four corresponding radiation beams, lie, two by two, in rectangular planes, symmetrically with respect to the focal axis of the paraboloid. v
A correcting device is placed in front of this arrange ment. This device comprises convergent flangesll', 12,
stantially smaller surfacetha'n the c'r'ojs s-section 'of the combined four guides; The coupling. between *the f windows 2.1 toZd is avoided by means of any conven-p.
tional device'such as quarter-wave traps 9 and 10, as
,shown in Figs. 3 and4; Fig. 5 shows diagrammatically and in cross-section the transmitting and receiving device of the invention. It comprises a parabolic reflector 15 and feeding guides 51, 54 and 52,53.
7 Since, according to the invention, only four radiators are used (instead of five), it is essential to provide a T.R. switching'system, adapted for correctly combining the transmitted energy-and dividing or re-arranging the received energy, as the case maybe.
This switching arrangement enables the system to pass from the transmitting position, the four guides being fed in phase, to the receiving position, where each of the guides operates independently of one another. The switching is provided, according to the invention, by jllIlClllOllS, T.R. and A.T.R. switches disposed as shown in Fig. 6. Four magic tees 55 to 58 are disposed between the radiating elements 1 to 4 and the energy source 69. i
When an ultra-high frequency pulse is transmitted, the energy supplied by source 69 is divided into two equal fractions by tee 55 each of these fractions being again divided into two. further equal fractionsby means of tees 56 and 57.
Each of the radiators thus receives substantially a quarter of the available energy, and the radiators are fed in-phase if the lengths of the guides connecting the 7 2,925,595 7 Patented Feb, 16,
respectively, it is easily found that these fractions are distributed as follows:
for tee 56: 1+2' in the arm connecting T56 to T55;
and- 1'2 in the arm connecting T56 to T58;
for tee 57: 3'+4' in the arm connecting T57 to T55;
and 34 in the arm connecting T57 to T58;
for tee 55: (1+2')+(3'+4') in the arm 67; and
(1+2)--(3+4') in the arm 60.
The sum of the voltages supplied by energies 1+2+3+4' is used in a receiver 72 connected to guide 68, the latter being coupled to guide 67 by duplexer 71, of a conventional type.
The difference (1+2)-(3+4) formed in arm 60 provides, as is well known, the error voltage corresponding to the angle of elevation of the target. This voltage is then used in a second receiver 73, connected to the vertical arm of tee 55 by means of T.R. device 63.
The sum (1'-2')+(3'-4') i.e. the difference (1+3')--(2'+4), collected in the horizontal arm of tee 58 provides a further error voltage which is used in a conventional manner in a third receiver '74, connected to guide 65 by T.R. device 64. Using such a set of three receivers is well known in the technic of monopulse radars.
It will be noted that the energy difference (l'+4')(2'+3') is collected in the vertical arm of tee 58; however, this difference is not used and is absorbed in a matched load 17.
Figure 7 shows a practical embodiment of the invention, wherein same reference numbers have been used to designate same elements as in the preceding figures.
Curves, shown in Figs. 8, 9 and 10, illustrate the results obtained during tests, with a frequency of 9,375 megacycles. This axis of the radiated beam is directed along the axis of the paraboloid reflector.
As shown in the diagram of Fig. 8 the aperture angle of the transmission beam, measured at a level of 3 db is 2 4' and at 10 db is less than 5.
As shown in Figs. 9 and 10, the four reception patterns intersect at a level of about 3 db. The aperture angles at 3 db and at 10 db were respectively 2 3 and less than 5.
What I claim is:
A transmitting and receiving device of the monopulse type, comprising: a reflector; and a first, a second, a third and a fourth rectangular radiator disposed side by side and having respectively, a first, a second, a third, and a fourth phase centers, said phase centers being located respectively at the four apices of a rectangle; said first, second, third and fourth radiators having respectively a first, a second, a third and a fourth resonant window directed towards said reflector, the respective distances between the centers of said windows being respectively smaller than the respective distances of said phase centers; the outer edges of said radiators thus forming a rectangle, and two pairs of flanges having outer edges converging by pairs, directed towards said reflector and forming the lateral walls of a truncated pyramid whose large base contacts said rectangle formed by said outer edges of said radiators and whose small base is defined by said outer edges of said flanges; and means for feeding in phase to said radiators the ultra high frequency pulse modulated energy to be transmitted, and for separately collecting the energy respectively received by each of said four radiators.
References Cited in thefile of this patent UNITED STATES PATENTS 2,585,173 Riblet Feb. 12, 1952
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1133058T | 1955-09-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2925595A true US2925595A (en) | 1960-02-16 |
Family
ID=9638666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US609151A Expired - Lifetime US2925595A (en) | 1955-09-21 | 1956-09-11 | Monopulse transmitting and receiving systems |
Country Status (3)
Country | Link |
---|---|
US (1) | US2925595A (en) |
FR (1) | FR1133058A (en) |
GB (1) | GB796915A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3093826A (en) * | 1960-04-08 | 1963-06-11 | Litton Systems Inc | Antenna system |
US3127494A (en) * | 1961-03-13 | 1964-03-31 | Studebaker Corp | Microwave heating apparatus |
US3129425A (en) * | 1957-09-27 | 1964-04-14 | Westinghouse Electric Corp | Three beam monopulse radar system and apparatus |
US3271776A (en) * | 1962-12-28 | 1966-09-06 | Hazeltine Research Inc | Intercoupling lines for impedance matching of array antennas |
US3308468A (en) * | 1961-05-22 | 1967-03-07 | Hazeltine Research Inc | Monopulse antenna system providing independent control in a plurality of modes of operation |
US3392395A (en) * | 1961-05-22 | 1968-07-09 | Hazeltine Research Inc | Monopulse antenna system providing independent control in a plurality of modes of operation |
US4348679A (en) * | 1980-10-06 | 1982-09-07 | United Technologies Corporation | Multi-mode dual-feed array radar antenna |
US4495504A (en) * | 1983-03-02 | 1985-01-22 | Raytheon Company | Radio frequency antenna having a reflector with an edge in a pattern null region to reduce edge scattering |
US4712110A (en) * | 1985-12-26 | 1987-12-08 | General Dynamics, Pomona Division | Five-port monopulse antenna feed structure with one dedicated transmit port |
FR2943466A1 (en) * | 2009-03-20 | 2010-09-24 | Thales Sa | Radiating element i.e. single pulse bipolarization radiating element, for e.g. Cassegrain reflector antenna of radar, has polarization filters set along direction parallel to dipole branches placed above plane of openings of waveguides |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1240951B (en) * | 1960-02-17 | 1967-05-24 | North American Aviation Inc | Radar antenna arrangement for the simultaneous determination of distance and direction in the azimuth and elevation plane |
US3241146A (en) * | 1963-01-30 | 1966-03-15 | North American Aviation Inc | Four aperture radiator for illuminating main dish |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2585173A (en) * | 1948-07-01 | 1952-02-12 | Raytheon Mfg Co | Radio-frequency transmission line circuit |
-
1955
- 1955-09-21 FR FR1133058D patent/FR1133058A/en not_active Expired
-
1956
- 1956-09-03 GB GB26862/56A patent/GB796915A/en not_active Expired
- 1956-09-11 US US609151A patent/US2925595A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2585173A (en) * | 1948-07-01 | 1952-02-12 | Raytheon Mfg Co | Radio-frequency transmission line circuit |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3129425A (en) * | 1957-09-27 | 1964-04-14 | Westinghouse Electric Corp | Three beam monopulse radar system and apparatus |
US3093826A (en) * | 1960-04-08 | 1963-06-11 | Litton Systems Inc | Antenna system |
US3127494A (en) * | 1961-03-13 | 1964-03-31 | Studebaker Corp | Microwave heating apparatus |
US3308468A (en) * | 1961-05-22 | 1967-03-07 | Hazeltine Research Inc | Monopulse antenna system providing independent control in a plurality of modes of operation |
US3392395A (en) * | 1961-05-22 | 1968-07-09 | Hazeltine Research Inc | Monopulse antenna system providing independent control in a plurality of modes of operation |
US3271776A (en) * | 1962-12-28 | 1966-09-06 | Hazeltine Research Inc | Intercoupling lines for impedance matching of array antennas |
US4348679A (en) * | 1980-10-06 | 1982-09-07 | United Technologies Corporation | Multi-mode dual-feed array radar antenna |
US4495504A (en) * | 1983-03-02 | 1985-01-22 | Raytheon Company | Radio frequency antenna having a reflector with an edge in a pattern null region to reduce edge scattering |
US4712110A (en) * | 1985-12-26 | 1987-12-08 | General Dynamics, Pomona Division | Five-port monopulse antenna feed structure with one dedicated transmit port |
FR2943466A1 (en) * | 2009-03-20 | 2010-09-24 | Thales Sa | Radiating element i.e. single pulse bipolarization radiating element, for e.g. Cassegrain reflector antenna of radar, has polarization filters set along direction parallel to dipole branches placed above plane of openings of waveguides |
Also Published As
Publication number | Publication date |
---|---|
FR1133058A (en) | 1957-03-20 |
GB796915A (en) | 1958-06-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3448450A (en) | Pulse radar for determining angles of elevation | |
US3482251A (en) | Transceive and tracking antenna horn array | |
US2432858A (en) | Antenna system | |
US2429601A (en) | Microwave radar directive antenna | |
US2810905A (en) | High frequency directive beam apparatus | |
US2925595A (en) | Monopulse transmitting and receiving systems | |
US5977904A (en) | Structure of aperture antenna and radar system using same | |
US2965898A (en) | Antenna | |
JPH0444441B2 (en) | ||
US2846678A (en) | Dual frequency antenna | |
US3325817A (en) | Dual frequency horn antenna | |
US2653238A (en) | Dual frequency antenna | |
US3158862A (en) | Wide-angle electrically-modulated reflector | |
US3311917A (en) | Stepped beam slot antenna array | |
US3828349A (en) | Stacked beam radar | |
US2918673A (en) | Antenna feed system | |
US2913723A (en) | Variable pattern radar aerial | |
US3471857A (en) | Planar array antenna arrangements | |
US3129425A (en) | Three beam monopulse radar system and apparatus | |
US3623094A (en) | Target acquisition antenna | |
US2458885A (en) | Directive antenna system | |
US3711858A (en) | Monopulse radar antenna structure | |
US3412405A (en) | Side lobe response reducing system | |
US2187618A (en) | Radio beacon system | |
US3196444A (en) | Interrogating antenna with control radiation |