JPS5897902A - Reflector type antenna device - Google Patents
Reflector type antenna deviceInfo
- Publication number
- JPS5897902A JPS5897902A JP19647781A JP19647781A JPS5897902A JP S5897902 A JPS5897902 A JP S5897902A JP 19647781 A JP19647781 A JP 19647781A JP 19647781 A JP19647781 A JP 19647781A JP S5897902 A JPS5897902 A JP S5897902A
- Authority
- JP
- Japan
- Prior art keywords
- frequency band
- angle
- antenna
- feeding
- reflector
- 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.)
- Granted
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q5/00—Arrangements for simultaneous operation of antennas on two or more different wavebands, e.g. dual-band or multi-band arrangements
- H01Q5/40—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements
- H01Q5/45—Imbricated or interleaved structures; Combined or electromagnetically coupled arrangements, e.g. comprising two or more non-connected fed radiating elements using two or more feeds in association with a common reflecting, diffracting or refracting device
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aerials With Secondary Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
Description
【発明の詳細な説明】
この発明はマイクロ波帯で用−られる反射鏡形アンテナ
装置に関し、二つ以上の多周波数帯で共用し、さらに周
波数帯によって多少異なる照射領域をカバーするアンテ
ナを提供するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a reflecting mirror antenna device used in the microwave band, and provides an antenna that can be used in two or more multiple frequency bands and further covers irradiation areas that differ somewhat depending on the frequency band. It is something.
一般にこの樵のアンテナは例えば人工衛星搭載用のアン
テナとして用いられ、一つの周波数帯のビームである地
域をカバーし、また他の周波数帯のビームで大部分はオ
ーバラップしているが少しずれた地域をカバーする必要
がある場合などに用匹られる。Generally, this woodcutter's antenna is used, for example, as an antenna onboard an artificial satellite, with a beam of one frequency band covering an area, and a beam of another frequency band, mostly overlapping but slightly shifted. They are used when it is necessary to cover an area.
従来の人工衛星搭載用の多周波数帯共用アンテナとして
は第1図に示すようなオフセットパラボラアンテナが多
く用いられて−る。すなわちオフセットパラボラ反射@
ill+の焦点に装炭ホーン(2)の位相中心を一致さ
せた構造のものであり、(31は開口径、(4)は給電
角、(5)は開口角である。ここで、多周波数帯を共用
する装炭ホーンの場合にはその位相中心点は最も利得を
高くしたい周&数帯に対するものである。As a conventional multi-frequency band antenna mounted on an artificial satellite, an offset parabolic antenna as shown in FIG. 1 is often used. That is, offset parabolic reflection @
It has a structure in which the phase center of the charging horn (2) coincides with the focal point of ill+, (31 is the aperture diameter, (4) is the feed angle, and (5) is the aperture angle. In the case of a charging horn that shares a band, the phase center point is for the circumference and several bands for which the highest gain is desired.
また、給電角(4)は反射鏡(1)、の開口角+51の
中心を見込む角度で給電して釣る。この場合には各周波
数帯での放射ビームの中心方向は大略一致し゛ている。Moreover, the feeding angle (4) is an angle that looks at the center of the aperture angle +51 of the reflecting mirror (1), and fishing is carried out by feeding electricity. In this case, the center directions of the radiation beams in each frequency band are approximately the same.
このため、第2図に示すようにある周波数帯での照射領
域(6)と他の周波数帯での照射領域(7)が異なる場
合には、アンテナの方向を照射領域16)の中心に一致
させると、この周波数帯での照射領域内最小利得は最大
になるが、照射領域(7)に対してはこの周波数帯のビ
ームの中心方向が照射領域(6)の中心にあるため、照
射領域内最小利得が低くなるという欠点があった。Therefore, as shown in Figure 2, if the irradiation area (6) in one frequency band is different from the irradiation area (7) in another frequency band, the direction of the antenna should be aligned with the center of the irradiation area 16). Then, the minimum gain within the irradiation area in this frequency band becomes maximum, but for the irradiation area (7), since the center direction of the beam in this frequency band is at the center of the irradiation area (6), the irradiation area The disadvantage is that the minimum gain within the range is low.
この発明はこの従来の欠点を解決するために。This invention aims to solve this conventional drawback.
多周波数帯共用−次ホーンの位相中心点が各周波数帯に
より異なっていることを利用して1反射鏡への給゛峨角
t−変えることにより9周波数帯によってアンテナの放
射ビームの方向を変えるもので、以下図面について詳細
に脱明する。Multi-frequency band sharing - Using the fact that the phase center point of the next horn is different for each frequency band, the direction of the antenna's radiation beam can be changed depending on the nine frequency bands by changing the feed angle t to one reflecting mirror. Therefore, the drawings will be explained in detail below.
第3図はこの発明の実施例であって、は】はオフナツト
パラボラ反射鏡、(2)は多周波数帯共用の装炭ホーン
、 Ialは反射鏡の開口径、(4)は給電角、(5)
は反射鏡の開口角、(8)は利得を最も高(した18波
帝での位相中心点、(9)は他の周波数帯の位相中心点
である。FIG. 3 shows an embodiment of the present invention, where is an off-nut parabolic reflector, (2) is a charging horn that can be used for multiple frequency bands, Ial is the aperture diameter of the reflector, and (4) is the feeding angle. (5)
is the aperture angle of the reflecting mirror, (8) is the phase center point at the 18th wave with the highest gain, and (9) is the phase center point for other frequency bands.
第3図において2位置中心点(8)の周波数帯では給電
角(4)に関係なくアンテナの放射ビームの方向は一定
であるが1位相中心点(9)の周波数帯では給電角(4
傅変化に従って0反射鏡の開口面上の位相分布が第3図
での上下方向で対称でなくなる。この結果アンテナの放
射ビームの方向も上下方向に変化することにおる。In Figure 3, in the frequency band of the 2nd position center point (8), the direction of the antenna radiation beam is constant regardless of the feeding angle (4), but in the frequency band of the 1st phase center point (9), the direction of the antenna radiation beam is constant regardless of the feeding angle (4).
As the value changes, the phase distribution on the aperture surface of the 0 reflecting mirror is no longer symmetrical in the vertical direction in FIG. As a result, the direction of the radiation beam of the antenna also changes in the vertical direction.
第4因は開口径(3)が21111.開口角(5)が9
0.3度のオフセットパラボラ反射鏡山で1周波数が2
5−1第4図(a)と5.925GHz第4図(b)の
場合について、給電角(4)t−変化した時の放射ノ(
ター/の計算例を示して−る。第4図(a)は周波数2
.5GHz。The fourth factor is the opening diameter (3) of 21111. Aperture angle (5) is 9
1 frequency is 2 with 0.3 degree offset parabolic reflector mountain
5-1 Regarding the cases of Fig. 4(a) and 5.925 GHz Fig. 4(b), the radiation noise when the feeding angle (4) t changes (
An example of calculation of ter/ is shown. Figure 4(a) shows frequency 2
.. 5GHz.
右旋円偏波での利得30dBの等高mt−示し、実線は
給電角55.2度の場合、破線は給電角6a、5度の場
合を示“す。また、第4図(b)は周波数5.925G
Hz。The contour mt of a gain of 30 dB in right-handed circularly polarized waves is shown. The solid line shows the case where the feeding angle is 55.2 degrees, and the broken line shows the case where the feeding angle is 6a, 5 degrees. Also, Fig. 4(b) is frequency 5.925G
Hz.
左旋円偏波での利得33di+の等高銀を示し、実線は
給電角55.2度の場合、破線は給電角65.5[の場
合を示す。この場合−次ホーy (21tj周波数2.
5GHzでの位相中心点(8)が反射鏡山の焦点に一致
しており1周波数5.925GIizの位相中心点(9
)は焦点からずれた位置にある。第4図から9周波数2
.5GHzでは給電角(4)の変化によっても、放射ビ
ームの中心方向はほとんど変化してすな−が。The graph shows a contour silver with a gain of 33di+ in left-handed circularly polarized waves, the solid line shows the case where the feeding angle is 55.2 degrees, and the broken line shows the case where the feeding angle is 65.5 degrees. In this case - order ho y (21tj frequency 2.
The phase center point (8) at 5 GHz coincides with the focal point of the reflecting mirror mountain, and the phase center point (9) at 1 frequency 5.925 GIiz
) is located out of focus. From Figure 4 9 Frequency 2
.. At 5 GHz, the center direction of the radiation beam hardly changes even if the feed angle (4) changes.
周波数5.925GHzの場谷には放射ビームの中心方
向は上下方向に約0.35度ずれていること力;わカム
る。なおこの時の放射ビームの中心方向での利得の変化
は周波数2.50ozで0.3dB、周、波数5.92
5GHzで0.7dBであった。At a frequency of 5.925 GHz, the center direction of the radiation beam is shifted by about 0.35 degrees in the vertical direction. At this time, the change in gain in the direction of the center of the radiation beam is 0.3 dB at a frequency of 2.50 oz, and the frequency and wave number are 5.92.
It was 0.7 dB at 5 GHz.
第5Nは他の実施例を示す側面構成図であり。No. 5N is a side configuration diagram showing another embodiment.
第6図は第5園の正面構成図であ゛る。多周波数帯共用
の装炭ホーン(21は反射鏡(11の焦点と、利得t−
最も高くしたい周波数帯の位相中心点+8)−1)E一
致していて、給電角(4)は反射鏡面+11の焦点を含
む対象面から、その直交方向に角度+11だけずらして
いる。この結果アンテナのビームの中心方向は2位相中
心点(8)に対しては1反射鏡(1)の正面方向になる
が9位相中心点(9)に対しては角度αC工って左右方
向にずれることになる。従って、左右方向に中心のずn
た2つの照射領域全2つの周波数帯で効率工〈カッ(−
すること力(できる、また、オフセラトノ(ラボラ反射
鍵形アンテナを周波数帯に工って旋回方向の異なる円偏
波で使用する場合には位相中心点+81と191が一致
していても、オフセット形反射d111で発生する交さ
偏波により、ビームの中心方向力;1反射鏡(1)の正
面方向に対して左右の互に反対方向にずれるという欠点
があるが、この発明によると位相中心点(8)の周波数
帯のビームの中心方向に対して、角度(1Gによって1
位相中心点(9)の周波数帯のビームの中心方向を左右
方向の所定の位置にすることができる。Figure 6 is a front view of the fifth garden. Charging horn (21 is a reflecting mirror (11's focal point and gain t-
The phase center point of the frequency band that is desired to be the highest coincides with +8)-1)E, and the feed angle (4) is shifted by an angle +11 in the orthogonal direction from the target plane including the focal point of the reflecting mirror surface +11. As a result, the center direction of the antenna beam is in the front direction of the 1st reflector (1) for the 2nd phase center point (8), but in the left-right direction by an angle αC for the 9th phase center point (9). It will shift to Therefore, the center deviation n in the left-right direction
Efficiency in all two irradiation areas and two frequency bands.
In addition, when using a laboratory reflective key antenna in a frequency band and using circularly polarized waves with different rotation directions, even if the phase center points +81 and 191 coincide, the offset type Due to the cross-polarized waves generated by the reflection d111, the force in the center direction of the beam is shifted in opposite directions on the left and right with respect to the front direction of the mirror (1), but according to this invention, the phase center point (8) Angle (1G by 1G) with respect to the center direction of the beam in the frequency band
The center direction of the beam in the frequency band of the phase center point (9) can be set at a predetermined position in the left-right direction.
第7図は他の実施例であって、 tillは回転対称な
パラボラ反射鏡であり、多周波数帯共用−次ホーン(2
)は反射fitllの焦点と、利得を殿も^くした一周
ea帝の位相中心点(8)が一致して−て。FIG. 7 shows another embodiment, in which till is a rotationally symmetrical parabolic reflector, and a multi-frequency band common -order horn (2
), the focal point of the reflection fitll and the phase center point (8) of the round ea, which greatly reduced the gain, coincide.
給電角a21は反射鏡(IIIの中心軸力1ら角度0z
だけずらしている。この結果アンテナのビームの中IC
?方向は9位相中心点(8)に対しては反射鏡(Ill
の正面方向になるが1位相中心点(9)に対しては、角
gu11によって反射鏡aDの正面方向力)らずれるこ
とになる、従って、中心のずれた2つの照射領域全2つ
の周波数で効率工〈カッ(−することカニできる。The feeding angle a21 is the angle 0z from the central axial force 1 of the reflecting mirror (III).
It's shifted by just that. As a result, the IC inside the beam of the antenna
? The direction is the reflector (Ill) for the 9 phase center point (8).
However, with respect to the 1 phase center point (9), the frontal force of the reflecting mirror aD is shifted by the angle gu11.Therefore, the frequencies of all two irradiation areas whose centers are shifted are Efficiency work〈cough (-) can be crab.
以上説明したように、この発明によると給電角(4)を
変化することにより1反射鏡山の焦点にある位相中心点
(8)の周波数での放射ビームの中心方向はほぼ一定の
t\で9位相中心点(91の周i21!数の放射ビーム
の中心方向を変えることができるので9周波数帯に1り
多少異なる照射領域の要求がある人工衛星搭載用等の多
周波数帯共用アンテナとして、照射領域内最小利得を高
くすることができるという利点がある。As explained above, according to the present invention, by changing the feeding angle (4), the central direction of the radiation beam at the frequency of the phase center point (8) at the focal point of one reflecting mirror mountain is changed at a substantially constant t\9. Since the center direction of the phase center point (91 circumference i21!) of the radiation beam can be changed, it can be used as a multi-frequency band antenna for use onboard artificial satellites, etc., which requires slightly different irradiation areas in 9 frequency bands. This has the advantage that the minimum gain within the region can be increased.
第1図は従来のアンテナの構成図、第2因は照射領域を
示す図、第3(8)はこの発明の一実施例を示すアンテ
ナの構成囚、第4図はこの発明の一実施例の効果を示す
アンテナの放射パターンを示す図、HS図はこの発明の
他の実施例を示す歯面構成図、第6肉は第5図の正面構
成図。
第7図はこの発明の他の実施例を示す#f構成図ある。
di・・・オフセットパラボラ反射鏡、 12+・・・
−次ホ−y、+31・・・開口径、(4)・・・給電角
、(5)・・・開口角。
+61. +71・・・照射領域、 +81. +91
・・・位相中心点、u−・回転対称形パラボラ反射−1
なお1図中同一あるいは相当部分には同一符号を付して
示しである。
第1図
\
第2図
第3図
、 ′Iヨ城
9コ
115図
第61!l
第7図Figure 1 is a configuration diagram of a conventional antenna, the second factor is a diagram showing the irradiation area, Figure 3 (8) is a configuration diagram of an antenna showing an embodiment of the present invention, and Figure 4 is an embodiment of the present invention. The HS diagram is a tooth surface configuration diagram showing another embodiment of the present invention, and the sixth figure is a front configuration diagram of FIG. 5. FIG. 7 is a block diagram of #f showing another embodiment of the present invention. di...offset parabolic reflector, 12+...
-th order ho-y, +31...Aperture diameter, (4)...Feeding angle, (5)...Aperture angle. +61. +71...irradiation area, +81. +91
...Phase center point, u--Rotationally symmetrical parabolic reflection-1 Note that the same or corresponding parts in Figure 1 are denoted by the same reference numerals. Figure 1 \ Figure 2 Figure 3, 'I Yo Castle 9 Ko 115 Figure 61! l Figure 7
Claims (1)
れる反射鏡形アンテナ装置において。 上記−次ホー/の位相中心を一つの周fi数帯について
パラボラ反射鏡の焦点に一致させ、他の周波数帯につい
てFi、焦点からずらし、かつ反射鏡への給電角を選ぶ
ことにより、アンテナからの放射ビームの方向を周波数
帯それぞれによってずらすようにしたことを特徴とする
反射鏡形アンテナ装置。[Claims] A reflector type antenna device comprising a parabolic reflector and a multi-frequency band common horn. By aligning the phase center of the -order Ho/ with the focus of the parabolic reflector for one frequency band, and shifting it from the focus of Fi for other frequency bands, and selecting the feeding angle to the reflector, the antenna can be A reflecting mirror antenna device characterized in that the direction of the radiation beam is shifted depending on each frequency band.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19647781A JPS5897902A (en) | 1981-12-07 | 1981-12-07 | Reflector type antenna device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19647781A JPS5897902A (en) | 1981-12-07 | 1981-12-07 | Reflector type antenna device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5897902A true JPS5897902A (en) | 1983-06-10 |
| JPH0131721B2 JPH0131721B2 (en) | 1989-06-27 |
Family
ID=16358442
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19647781A Granted JPS5897902A (en) | 1981-12-07 | 1981-12-07 | Reflector type antenna device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5897902A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0739812U (en) * | 1991-09-20 | 1995-07-18 | 博康 山田 | Lower limb traction device |
| JP2008131575A (en) * | 2006-11-24 | 2008-06-05 | Sharp Corp | Feed horn, satellite receiving converter and sanitary receiving antenna |
-
1981
- 1981-12-07 JP JP19647781A patent/JPS5897902A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0131721B2 (en) | 1989-06-27 |
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