WO2002071540A1 - Antenne a reflecteur - Google Patents
Antenne a reflecteur Download PDFInfo
- Publication number
- WO2002071540A1 WO2002071540A1 PCT/JP2002/001863 JP0201863W WO02071540A1 WO 2002071540 A1 WO2002071540 A1 WO 2002071540A1 JP 0201863 W JP0201863 W JP 0201863W WO 02071540 A1 WO02071540 A1 WO 02071540A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- reflector
- antenna
- axis
- antenna device
- mirror
- Prior art date
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
- H01Q19/18—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces
- H01Q19/19—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
- H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
- H01Q19/18—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces
- H01Q19/19—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface
- H01Q19/193—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface with feed supported subreflector
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
- H01Q3/08—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/12—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems
- H01Q3/16—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device
- H01Q3/20—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical relative movement between primary active elements and secondary devices of antennas or antenna systems for varying relative position of primary active element and a reflecting device wherein the primary active element is fixed and the reflecting device is movable
Definitions
- the present invention relates to a reflector antenna device, and more particularly to a reflector antenna device that performs scanning by rotating around two axes perpendicular to each other.
- This reflector antenna device usually has a reflector having a sub-reflector receiving irradiation of electromagnetic waves from a radiator, and a main reflector reflecting the electromagnetic waves reflected from the sub-reflector and directing the target to a target.
- An axially symmetric Cassegrain antenna having not only a height in the azimuth axis direction of the reflector antenna device but also a length dimension in the elevation axis direction and a width dimension in a direction perpendicular thereto. Also, since the elevation rotation center axis does not pass through the reflecting mirror but passes through a position away from the reflecting mirror, changing the direction (angle) of the reflecting mirror inevitably changes its position. Therefore, it was necessary to increase the working area of the reflector of the antenna device, and a large space was required for installing the reflector antenna device.
- the conventional reflector antenna device when there is a requirement to install a reflector antenna device in a limited, relatively small space, such as when it is mounted on an aircraft, the conventional reflector antenna device has a large operating area for the reflector described above. could not. It has also been proposed that small antenna elements are fixedly arranged in an array to reduce the height, and that the directivity of the antenna elements be electrically controlled for scanning. The equipment for this is extremely expensive and is of little practical use.
- an object of the present invention is to provide a reflector antenna device which can be installed in a small space, has sufficient practicality, and performs scanning by rotating around two axes perpendicular to each other. Disclosure of the invention
- means for solving the above-mentioned problems are as follows.
- the elevation axis is the azimuth axis of the reflector.
- the reflector has a substantially rectangular opening extending in the direction of the elevation axis, passing through a position substantially at the center of the direction and substantially at the center of the reflection mirror in a direction perpendicular to the elevation axis.
- the mirror surface is modified so that it receives and reflects substantially all of the supplied electromagnetic wave, so that the antenna height does not increase even when the above-mentioned reflecting mirror rotates around the elevation axis. This is the characteristic reflector antenna device.
- the reflector may include a sub-reflector that receives electromagnetic waves from the radiator, and a main reflector that reflects the electromagnetic waves reflected from the sub-reflector and directs the target toward a target. it can.
- the height of the antenna including a part of the power feeding device rotated simultaneously with the reflector antenna may be prevented from increasing.
- the reflecting mirror may be a reflecting mirror array including a plurality of reflecting mirror elements arranged with the elevation axes aligned.
- Each of the reflector antennas of the main reflector has a substantially rectangular aperture shape, and in order to suppress grating lobes, each reflector antenna has a rectangular aperture when viewed from the mirror axis direction.
- the mirror surface was modified so that the electromagnetic field distribution at the aperture became a nearly uniform distribution.
- the radiator has a mirror surface set parallel to the azimuth rotation plane, and the center axis of the radiator is aligned with the elevation axis.
- the mirror surface is set so that the sub-reflector does not block when viewed from the mirror axis direction.
- the reflector antenna is a Cassegrain antenna.
- the reflector antenna is a Gregorian antenna.
- FIG. 1 is a schematic side view showing a reflector antenna device according to one embodiment of the present invention.
- FIG. 2 is a schematic top view showing the reflector antenna device of FIG.
- FIG. 3 is a schematic front view showing the reflector antenna device of FIG.
- FIG. 4 is a schematic front view showing an array-type reflector antenna device according to another embodiment of the present invention.
- FIG. 5 is a schematic side view showing an array-type reflector antenna device according to a third embodiment of the present invention.
- FIG. 6 is a schematic top view showing the reflector antenna device of FIG.
- FIG. 7 is a schematic enlarged front view showing the reflector antenna of the reflector antenna device of FIG.
- FIG. 8 is a schematic side view showing an array-type reflecting mirror antenna device according to a fourth embodiment of the present invention.
- FIG. 9 is a schematic top view showing the reflector antenna device of FIG.
- FIG. 10 is a schematic side view showing a reflector antenna of a reflector antenna device according to a fifth embodiment of the present invention.
- FIG. 11 is a schematic side view showing an array-type reflector antenna device according to a sixth embodiment of the present invention.
- FIG. 12 is a schematic top view showing the reflector antenna device of FIG.
- FIG. 13 is a schematic side view showing an array-type reflector antenna device according to a seventh embodiment of the present invention.
- FIG. 14 is a schematic top view showing the reflector antenna device of FIG.
- FIG. 15 is a schematic side view showing a reflector antenna device according to an eighth embodiment of the present invention.
- Embodiment 1 of a reflector antenna device is shown in FIGS.
- the reflector antenna device includes a reflector 1 and an And a rotation mechanism 4 that rotates around the rotation axis 2 and the elevation axis 3.
- the reflecting mirror 1 includes a sub-reflecting mirror 6 receiving electromagnetic waves from a radiator 5 that emits electromagnetic waves, and a main reflecting device that reflects the electromagnetic waves reflected from the sub-reflecting mirror 6 and directs the waves toward a target (not shown).
- Mirror 7 is provided.
- the sub-reflector 6 is supported by the support mechanism 8 in a state where the sub-reflector 6 is axially aligned with a distance from the main reflector 7.
- the reflecting mirror 1 is supported by a rotation support mechanism 9 so as to be rotatable around the rotation axis 3 with respect to the turntable 10, and is rotated by the rotation drive source 11.
- the first mouth joint 13 is connected to the feeder 12 at a position on the elevation axis 3. Have been purchased.
- the reflecting mirror 1 thus supported so as to be able to rotate about the elevation axis 3 with respect to the rotary table 10 is also supported so that the rotary table 10 can be rotated about the azimuth axis 2. It can be rotated around the azimuth axis 2 by the rotary drive source 14 together with the rotary table 10.
- a feed line 12 connecting the feed device 15 and the radiator 5 includes a second joint 1 at the rotation center of the turntable 10, that is, at a position on the azimuth axis 2 of the reflector 1. 6 is provided so that the rotary table 10 and the reflecting mirror 1 thereon can be allowed to rotate around the azimuth axis 2 at this portion.
- the reflecting mirror 1 has a main reflecting mirror 7 and a sub-reflecting mirror 6, but has a length D (see FIGS. 1 and 2) in the direction of the elevation axis 3 as a whole.
- the antenna has a width of W (see Figs. 2 and 3) in a direction perpendicular to the one-way axis 3 and has a substantially rectangular aperture.
- the elevation axis 3 is the azimuth axis 2 direction of the reflector 1.
- the range in which 1 moves that is, the operation area S, is inside the circle Y drawn by the outermost edge of the main reflecting mirror 7 about the elevation axis 3 as shown in FIG.
- the operating area S represented by the circle Y is extremely large compared to, for example, the antenna described in the aforementioned Wakana paper.
- the antenna height is small even when the reflector is rotated around the elevation axis.
- the main reflecting mirror 7 and the sub-reflecting mirror 6 of the reflecting mirror 1 are each mirror-polished so as to receive and reflect substantially all of the electromagnetic waves supplied to the reflecting mirror 1.
- Mirror modification is a method for controlling the antenna aperture shape and antenna aperture distribution. For example, see IEE Proc. Microw. Antennas Propag. Vol. 146, No. l, pp. 60-64, 1999, etc. Described.
- the antenna has been modified so that the aperture shape is substantially rectangular, and the mirror surface has been modified so that the aperture distribution is uniform.
- the radio wave radiated from the primary radiator 5 is reflected by the sub-reflector 6, and the reflected radio wave is reflected by the main reflector 7 and directed to a target (not shown).
- a target not shown.
- the main reflecting mirror 7, the sub-reflecting mirror 6, the supporting mechanism 8 for the sub-reflecting mirror, the primary radiator 5, and the first part 1 2a of the feed line 12 rotate about the elevation rotation axis 3. be able to.
- the power supply path 1 2a is connected to the second part 12 via the rotary joint 13 so that power can be supplied to the primary size scale 5 even when the antenna rotates around the elevation axis 3. .
- Fig. 2 is a view of the reflector antenna device viewed from above (from the mirror axis direction).
- this reflector antenna device In order to prevent the antenna height from increasing even when scanning in the elevation direction, this reflector antenna device must have not only the antenna height H but also the size in the direction perpendicular to the elevation axis 3 and the mirror axis (azimuth axis 2) of the antenna. (Width)
- the antenna is designed so that W becomes small.
- the design procedure of the reflector antenna device consists of the following two steps.
- the antenna height H including the main reflector 7 and the sub-reflector 6 is the highest at the same aperture diameter. This is a condition for lowering.
- Mirror modification is a technique for controlling the shape of the antenna aperture and the antenna aperture distribution.For example, IEE Proc. Micro. Antennas Propag. Vol. 146, No. l, P. 60- 64, 1999. By modifying the mirror surface, various antenna aperture shapes and aperture distributions can be realized.
- Figure 3 shows the antenna realized when the antenna is designed using the above-described method, as viewed from the direction of the elevation axis 3.
- the antenna does not go out of the fixed circle Y centered on the rotation axis 3 and can realize a low antenna height.
- the aperture aperture D of the antenna the antenna gain and the beam width in the azimuth direction can be adjusted.
- the aperture distribution of the antenna can be controlled to adjust the antenna gain and beam width.
- This antenna has the effect that it can be applied even when it is rotated around the elevation axis 3 and the antenna height is low, and there are restrictions on where the antenna is installed.
- FIG. 4 shows the characteristics of the reflector antenna device of the present invention.
- the feeder was placed below the azimuth-rotating joint, but some feeder circuits 16a and other parts 16b may have the above-mentioned joints depending on the antenna configuration. Azimuth and elevator at the same time as the main reflector
- This antenna device can be used to construct an antenna including the necessary parts. There is an effect that the height of the corner can be suppressed.
- FIG. 5 is a side view and FIG. 6 is a top view of another embodiment of the reflector antenna device of the present invention.
- the same or corresponding parts as those shown in FIGS. 1 to 3 are denoted by the same reference numerals, and their description is omitted.
- Some of them are: 1 is a reflecting mirror, 7 is a main reflecting mirror, 6 is a sub-reflecting mirror, 8 is a supporting mechanism of a sub-reflecting mirror, 5 is a primary radiator, 1 is a feed line, 2 is an azimuth axis
- Reference numeral 3 denotes an elevation rotation axis
- reference numerals 13 and 16 denote rotary joints
- reference numeral 10 denotes a rotary table.
- the antenna can rotate about two axes, around the azimuth axis 2 and around the elevation axis 3, and its mechanism is the same as that of the reflector antenna device of the above-described embodiment.
- this reflector antenna device not one reflector (antenna), but an antenna configuration using two antenna elements 1, that is, two Cassegrain antennas.
- the rotation about the azimuth axis 2 does not mean that each antenna element 1 rotates individually, but that the antenna element 1 supported on the turntable 10 rotates as a whole array.
- the lowest antenna in the posture where the antenna is not scanned is 1 of the antenna diameter. Therefore, an antenna that is half the size in three directions of the elevation axis of the antenna has half the height. By arranging two of these antennas in the three directions of the elevation axis to form an array antenna, the entire antenna is
- the antenna height can be made lower than that of the previous embodiment, and there is an effect that the present invention can be applied even when the dimensional installation environment of the reflector-device is more severe.
- grating lobes generated due to the use of a two-element array antenna that is usually several wavelengths away are suppressed.
- a mirror finish is applied as shown in Fig.7.
- 7a is the main reflector before the mirror surface modification
- 6a is the sub-reflector before the mirror surface modification
- 7b is the main reflector after the mirror surface modification
- 6b is the sub-reflector after the mirror surface modification.
- FIG. 8 is a side view and FIG. 9 is a top view of the reflector antenna device according to the present invention.
- 1 is a reflecting mirror
- 7 is a main reflecting mirror
- 6 is a sub-reflecting mirror
- 8 is a support mechanism for a sub-reflecting mirror
- 5 is a primary radiator
- 1 2 is a feed path
- 3 is an elevation rotation axis
- Reference numerals 3 and 16 denote a joint and a rotary table.
- the reflecting mirror 1 can rotate about two axes, an azimuth axis and an elevation axis, and the mechanism is the same as in the previous embodiment.
- an array antenna configuration using two offset Cassegrain antennas is used.
- the influence of blocking due to the sub-reflector can be reduced, the characteristics of the antenna such as the side lobe level can be improved, and not only the dimensional restrictions but also the This has the effect that it can be applied even when the antenna specifications are severe.
- FIG. 10 shows a side view of a reflector antenna device according to still another embodiment of the present invention.
- 1 is a reflector
- 7 is a main reflector
- 6 is a sub-reflector
- 8 is a support mechanism for a sub-reflector
- 5 is a primary radiator
- 1 is a feeder
- 2 is an azimuth axis
- 3 is an elevation rotation axis
- 16 is a mouth-evening joint
- 10 is a rotary table.
- a mirror surface is designed so that the direction of the primary radiator 5 is parallel to the azimuth rotation plane.
- the primary radiator 5 is The rotation of the primary radiator 5 during the rotation of the elevation is not required. Further, since the power supply path 12 for supplying power to the two primary radiators 5 can be connected without bending, the structure can be simplified. In addition, there is an effect that the structural load is small when driven mechanically.
- FIG. 11 is a side view and FIG. 12 is a top view of the reflector antenna device according to the present invention.
- the same or corresponding components as those shown in FIGS. 1 to 3 are denoted by the same reference numerals, and their description is omitted.
- Some of them are: 1 is a reflecting mirror, 7 is a main reflecting mirror, 6 is a sub-reflecting mirror, 8 is a supporting mechanism of a sub-reflecting mirror, 5 is a primary radiator, 1 is a feed line, 2 is an azimuth axis , 3 is an elevation rotation axis, 16 is a mouth-to-mouth joint, and 10 is a rotary table.
- the reflector antenna device of this embodiment is basically the same as that of the previous embodiment, but when viewed from the direction of the azimuth axis 2 (mirror axis), the shadow by the sub-reflector 6 does not block. This is a mirror surface design. In this embodiment, the effect of blocking by the sub-reflector 6 can be eliminated, and there is an effect that the characteristics of the antenna such as the level of the cyclone can be improved.
- FIG. 13 is a side view and FIG. 14 is a top view of the reflector antenna device according to the present invention.
- the same or corresponding components as those shown in FIGS. 1 to 3 are denoted by the same reference numerals, and their description is omitted.
- Some of them are: 1 is a reflecting mirror, 7 is a main reflecting mirror, 6 is a sub-reflecting mirror, 8 is a supporting mechanism of a sub-reflecting mirror, 5 is a primary radiator, 1 is a feed line, 2 is an azimuth axis
- Reference numeral 3 denotes an elevation rotation axis
- reference numerals 13 and 16 denote a rotary joint
- reference numeral 10 denotes a rotary table.
- FIGS. 13 and 14 show examples of the reflector 1 having an array antenna configuration using four offset Cassegrain antennas.
- the aperture diameter of each offset Cassegrain antenna is reduced. Since the height can be reduced, there is an effect that the antenna height of the reflector 1 of the reflector antenna device that can be realized can be further reduced.
- FIG. 15 is a side view of a reflector antenna device according to still another embodiment of the present invention.
- 1 is a reflector
- 7 is a main reflector
- 6 is a sub-reflector
- 8 is a support mechanism for a sub-reflector
- 5 is a primary radiator
- 1 is a feeder
- 2 is an azimuth axis
- Reference numeral 3 denotes an elevation rotation axis
- reference numerals 13 and 16 denote mouth joints
- reference numeral 10 denotes a rotary table.
- an antenna structure using one or a plurality of force segrain antennas as the reflecting mirror 1 is used.
- a reflection structure in which a Gregorian antenna is applied to an antenna structure having a similar structure is used as a whole. It is a mirror antenna device.
- FIG. 15 shows a reflector antenna device in which a Gregorian antenna is applied to the reflector antenna device of the fourth embodiment.
- the effects of the reflector antenna device of the present invention are as follows.
- the elevation axis is the azimuth axis of the reflector. Passing through a position substantially at the center of the direction and substantially at the center of the reflection mirror in a direction perpendicular to the elevation axis, the reflection mirror has a substantially rectangular opening long in the direction of the elevation axis, and However, the mirror surface is modified so as to receive substantially all of the supplied electromagnetic waves, so that the antenna height does not increase even when the reflecting mirror rotates around the elevation axis. Therefore, it is possible to provide a reflector antenna device that can be installed in a small space, has sufficient practicality, and performs scanning by rotating around two axes perpendicular to each other.
- the reflecting mirror may include a sub-reflecting mirror that receives the electromagnetic wave from the radiator, and a main reflecting mirror that reflects the electromagnetic wave reflected from the sub-reflecting mirror and directs the target to a target. Because it can be installed in a small space, It is possible to provide an efficient reflector antenna device that has sufficient practicality and performs scanning by rotating around two axes perpendicular to each other.
- the antenna height was not increased, including the part of the feeder that was rotated simultaneously with the reflector antenna. This has the effect that the height of the antenna can be reduced.
- the reflector may be a reflector array having a plurality of reflector elements arranged with the elevation axes aligned, so that the antenna height can be further reduced, and a small space can be obtained. It is possible to provide a reflector antenna device that can be installed in a room, has sufficient practicality, and scans by rotating around two axes perpendicular to each other.
- Each of the reflector antennas of the main reflector has a substantially rectangular aperture shape, and in order to suppress grating lobes, each reflector antenna has a rectangular aperture when viewed from the mirror axis direction.
- the mirror surface has been modified so that the electromagnetic field distribution at the aperture is a nearly uniform distribution. Therefore, the height of the antenna can be further reduced, the antenna can be installed in a small space, and there is sufficient practicality, and a highly efficient reflector that scans by rotating around two axes perpendicular to each other is provided.
- An antenna device can be provided.
- the radiator has a mirror surface set parallel to the azimuth rotation plane, and the center axis of the radiator is aligned with the elevation axis. Therefore, it is possible to provide a reflector antenna device that can be installed in a small space, has sufficient practicality, and has a simple configuration.
- the mirror surface is set so that the sub-reflector does not block when viewed from the mirror axis direction. Therefore, it is possible to provide a reflector antenna device that can be installed in a small space, has sufficient practicality, and does not cause blocking.
- the reflector antenna is a Cassegrain antenna, it can be installed in a small space, and a highly efficient reflector antenna device having sufficient practicality can be provided.
- the reflector antenna device according to the present invention is particularly useful as a reflector antenna device that performs scanning while rotating around two axes perpendicular to each other.
Landscapes
- Aerials With Secondary Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2002570345A JP3788784B2 (ja) | 2001-03-02 | 2002-02-28 | 反射鏡アンテナ装置 |
US10/275,064 US6741216B2 (en) | 2001-03-02 | 2002-02-28 | Reflector antenna |
EP02701640A EP1365473B1 (en) | 2001-03-02 | 2002-02-28 | Reflector antenna |
DE60204946T DE60204946T2 (de) | 2001-03-02 | 2002-02-28 | Reflektorantenne |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2001-58811 | 2001-03-02 | ||
JP2001058811 | 2001-03-02 | ||
PCT/JP2001/006236 WO2002071538A1 (fr) | 2001-03-02 | 2001-07-18 | Antenne a reflecteur |
JPPCT/JP01/06236 | 2001-07-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002071540A1 true WO2002071540A1 (fr) | 2002-09-12 |
Family
ID=26345115
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2002/001863 WO2002071540A1 (fr) | 2001-03-02 | 2002-02-28 | Antenne a reflecteur |
Country Status (4)
Country | Link |
---|---|
US (1) | US6741216B2 (ja) |
JP (1) | JP3788784B2 (ja) |
DE (1) | DE60204946T2 (ja) |
WO (1) | WO2002071540A1 (ja) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004091051A1 (ja) * | 2003-04-04 | 2004-10-21 | Mitsubishi Denki Kabushiki Kaisha | アンテナ装置 |
JP2008502207A (ja) * | 2004-06-02 | 2008-01-24 | ザ・ボーイング・カンパニー | 掃引円弧を最小化する、回転反射鏡アンテナを取り付ける方法および装置 |
JP2008510441A (ja) * | 2004-08-12 | 2008-04-03 | ザ・ボーイング・カンパニー | スイープされたアークを最小限にするための回転リフレクタアンテナを搭載するための方法および装置 |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4468300B2 (ja) * | 2003-08-13 | 2010-05-26 | 三菱電機株式会社 | 反射鏡アンテナ装置 |
US6999044B2 (en) * | 2004-04-21 | 2006-02-14 | Harris Corporation | Reflector antenna system including a phased array antenna operable in multiple modes and related methods |
JP4337877B2 (ja) * | 2004-05-21 | 2009-09-30 | 株式会社村田製作所 | アンテナ装置およびこれを用いたレーダ装置 |
US20060250316A1 (en) * | 2005-05-06 | 2006-11-09 | Space Systems/Loral, Inc. | Selectable subreflector configurations for antenna beam reconfigurability |
US7242360B2 (en) * | 2005-11-14 | 2007-07-10 | Northrop Grumman Corporation | High power dual band high gain antenna system and method of making the same |
US8914258B2 (en) * | 2011-06-28 | 2014-12-16 | Space Systems/Loral, Llc | RF feed element design optimization using secondary pattern |
US9899745B2 (en) * | 2013-09-13 | 2018-02-20 | Raytheon Company | Low profile high efficiency multi-band reflector antennas |
EP3657601B1 (en) * | 2014-06-27 | 2022-08-03 | ViaSat Inc. | Method of rotationally coupling antennas |
CN112563725B (zh) * | 2020-12-10 | 2021-08-24 | 华兴通信技术有限公司 | 无线微波通信装置 |
WO2023017249A1 (en) * | 2021-08-07 | 2023-02-16 | Techapp Consultants Limited | Antenna systems |
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JPH01235402A (ja) * | 1988-03-16 | 1989-09-20 | Fujitsu Ltd | オフセット形アンテナ装置 |
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JPS51130143A (en) * | 1975-05-08 | 1976-11-12 | Kokusai Denshin Denwa Co Ltd <Kdd> | Antenna unit |
US4186402A (en) * | 1976-05-18 | 1980-01-29 | Mitsubishi Denki Kabushiki Kaisha | Cassegrainian antenna with beam waveguide feed to reduce spillover |
DE2628713C2 (de) * | 1976-06-25 | 1987-02-05 | Siemens AG, 1000 Berlin und 8000 München | Rotationssymmetrische Zweispiegelantenne |
US6043788A (en) * | 1998-07-31 | 2000-03-28 | Seavey; John M. | Low earth orbit earth station antenna |
FR2787926B1 (fr) * | 1998-12-23 | 2001-02-09 | Cahors App Elec | Procede et dispositif de pointage et de positionnement d'une antenne multisatellite |
US6243047B1 (en) * | 1999-08-27 | 2001-06-05 | Raytheon Company | Single mirror dual axis beam waveguide antenna system |
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2002
- 2002-02-28 JP JP2002570345A patent/JP3788784B2/ja not_active Expired - Lifetime
- 2002-02-28 US US10/275,064 patent/US6741216B2/en not_active Expired - Lifetime
- 2002-02-28 DE DE60204946T patent/DE60204946T2/de not_active Expired - Lifetime
- 2002-02-28 WO PCT/JP2002/001863 patent/WO2002071540A1/ja active IP Right Grant
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JPS5467743A (en) * | 1977-11-09 | 1979-05-31 | Kokusai Denshin Denwa Co Ltd | Earth station antenna |
JPS62140465U (ja) * | 1986-02-26 | 1987-09-04 | ||
JPH01235402A (ja) * | 1988-03-16 | 1989-09-20 | Fujitsu Ltd | オフセット形アンテナ装置 |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004091051A1 (ja) * | 2003-04-04 | 2004-10-21 | Mitsubishi Denki Kabushiki Kaisha | アンテナ装置 |
JP2004312270A (ja) * | 2003-04-04 | 2004-11-04 | Mitsubishi Electric Corp | アンテナ装置 |
US7095380B2 (en) | 2003-04-04 | 2006-08-22 | Mitsubishi Denki Kabushiki Kaisha | Antenna device |
JP2008502207A (ja) * | 2004-06-02 | 2008-01-24 | ザ・ボーイング・カンパニー | 掃引円弧を最小化する、回転反射鏡アンテナを取り付ける方法および装置 |
JP2008510441A (ja) * | 2004-08-12 | 2008-04-03 | ザ・ボーイング・カンパニー | スイープされたアークを最小限にするための回転リフレクタアンテナを搭載するための方法および装置 |
Also Published As
Publication number | Publication date |
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DE60204946D1 (de) | 2005-08-11 |
JP3788784B2 (ja) | 2006-06-21 |
US20030151558A1 (en) | 2003-08-14 |
US6741216B2 (en) | 2004-05-25 |
JPWO2002071540A1 (ja) | 2004-07-02 |
DE60204946T2 (de) | 2006-05-11 |
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