JPH0514050A - Antenna system - Google Patents

Antenna system

Info

Publication number
JPH0514050A
JPH0514050A JP19261891A JP19261891A JPH0514050A JP H0514050 A JPH0514050 A JP H0514050A JP 19261891 A JP19261891 A JP 19261891A JP 19261891 A JP19261891 A JP 19261891A JP H0514050 A JPH0514050 A JP H0514050A
Authority
JP
Japan
Prior art keywords
antenna
main
sub
hole
reflecting mirror
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.)
Pending
Application number
JP19261891A
Other languages
Japanese (ja)
Inventor
Yutaka Shimawaki
豊 島脇
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP19261891A priority Critical patent/JPH0514050A/en
Publication of JPH0514050A publication Critical patent/JPH0514050A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To realize the antenna system having a high angle measuring accuracy with less effect by self weight deformation by installing a sub antenna to a side opposite to a radio wave radiation direction of a main antenna. CONSTITUTION:A sub antenna 2 is installed to a side opposite to a radio wave radiation direction of a main antenna 1. In this case, since a hole 11 is provided to a main reflecting mirror 3, though a beam shift is caused to the main antenna, a hole 12 of the same size is made to a position symmetrical to the position of the hole 11 with respect to the sub antenna, or only the hole 11 is formed and a frequency selecting mirror surface to reflect a radio wave of the main antenna and to transmit the radio wave of the sub antenna is provided to the position.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】この発明は、ロケットや衛星等を
追尾するアンテナ装置に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an antenna device for tracking a rocket or satellite.

【0002】[0002]

【従来の技術】図3は、例えば特開昭63−10730
3号公報に示された従来のアンテナ装置を示す平面図で
あり、図において、1は主アンテナ、2はこの主アンテ
ナ1と同一放射方向となるように主アンテナ1の外側に
設けた副アンテナ2である。副アンテナ2は主アンテナ
1に比して指向性及び利得の小さいアンテナである。
2. Description of the Related Art FIG. 3 shows, for example, Japanese Patent Laid-Open No. 63-10730.
FIG. 4 is a plan view showing a conventional antenna device disclosed in Japanese Patent Laid-Open No. 3 publication, in which 1 is a main antenna and 2 is a sub-antenna provided outside the main antenna 1 so as to have the same radiation direction as the main antenna 1. It is 2. The sub antenna 2 is an antenna having a directivity and a gain smaller than those of the main antenna 1.

【0003】次に動作について説明する。副アンテナ2
は主アンテナ1のビームに比べビーム幅が広いため、副
アンテナ2を用いて追尾し、同一放射方向を持つ主アン
テナ1の方向調整を行う。この特開昭63−10730
3号公報ではディジタル無線通信に適用するアンテナと
して、主アンテナ1は直径3.6mのパラボラアンテ
ナ、副アンテナ2は直径30cmのパラボラアンテナを
用いる例が紹介されている。
Next, the operation will be described. Sub antenna 2
Since the beam width is wider than the beam of the main antenna 1, the secondary antenna 2 is used for tracking to adjust the direction of the main antenna 1 having the same radiation direction. This Japanese Patent Laid-Open No. 63-10730
As an antenna applied to digital radio communication, Japanese Patent Laid-Open No. 3 discloses an example in which the main antenna 1 is a parabolic antenna having a diameter of 3.6 m and the sub-antenna 2 is a parabolic antenna having a diameter of 30 cm.

【0004】[0004]

【発明が解決しようとする課題】ところで、上記公報に
示されたアンテナ装置を、例えばロケット追尾レーダと
して用いるとすると、回線設計上、主アンテナ1は直径
5〜20m程度の大口径アンテナ、副アンテナ2は直径
0.3〜2m程度のアンテナが必要となる。
If the antenna device disclosed in the above publication is used, for example, as a rocket tracking radar, the main antenna 1 has a large diameter antenna having a diameter of about 5 to 20 m and a sub antenna because of the line design. 2 requires an antenna with a diameter of about 0.3 to 2 m.

【0005】また、主アンテナ1は方位角0°〜360
°,仰角0°〜90°の全天駆動追尾する必要があり、
上記のように主アンテナ1の外側に副アンテナ2を設け
る場合、仰角変化時の自重変形が大きくなり、測角精度
が低下するという問題があった。
Further, the main antenna 1 has an azimuth of 0 ° to 360 °.
Angle, elevation angle 0 ° ~ 90 ° It is necessary to track all sky driving,
When the sub-antenna 2 is provided outside the main antenna 1 as described above, there is a problem that the self-weight deformation becomes large when the elevation angle changes, and the angle measurement accuracy deteriorates.

【0006】即ち、ロケットを追尾するレーダに用いる
アンテナは開口径が大きく、ビーム幅が狭いため、捕捉
用の小開口径でビーム幅が広い副アンテナが必要となる
が、副アンテナを主アンテナの外側に密接して設置する
場合、仰角変化時の自重変形が大きくなるという問題が
あった。
That is, since an antenna used in a radar for tracking a rocket has a large aperture diameter and a narrow beam width, a sub-antenna with a small aperture diameter and a wide beam width is required for capturing. When installed close to the outside, there is a problem that the self-weight deformation becomes large when the elevation angle changes.

【0007】この発明は、上記のような問題点を解消す
るためになされたもので、主アンテナ内に副アンテナを
設置した上で主アンテナの仰角変化時の自重変形が小さ
く、高い測角精度を有するアンテナ装置を得ることを目
的としている。
The present invention has been made in order to solve the above problems, in which a sub-antenna is installed in the main antenna and the deformation of the main antenna due to its own weight when the elevation angle changes is small, resulting in high angle measurement accuracy. It is intended to obtain an antenna device having

【0008】[0008]

【課題を解決するための手段】この発明に係るアンテナ
装置は、主アンテナの主反射鏡の電波放射方向と反対側
の面内に捕捉アンテナとして用いる副アンテナを設置
し、副アンテナを設置するために主アンテナの主反射鏡
面に設けた穴と同じ大きさの穴を、主反射鏡上の中心に
関して点対称な位置に設けたものである。
In the antenna device according to the present invention, a sub-antenna used as a capture antenna is installed in the surface of the main antenna opposite to the radio wave radiation direction of the main reflector, and the sub-antenna is installed. In addition, a hole having the same size as the hole provided on the main reflecting mirror surface of the main antenna is provided at a position symmetrical with respect to the center on the main reflecting mirror.

【0009】また、副アンテナを設置するために主アン
テナの主反射鏡面に設けた穴に、周波数選択鏡面を設け
るようにしたものである。
Further, the frequency selective mirror surface is provided in the hole provided in the main reflecting mirror surface of the main antenna for installing the sub antenna.

【0010】[0010]

【作用】この発明におけるアンテナ装置は、主アンテナ
の主反射鏡の電波放射方向と反対側の面内に捕捉用の副
アンテナを設置するため、主反射鏡面に穴をあける必要
があり、このままでは主アンテナはビームシフト,利得
低下を生じるが、ロケット追尾用レーダでは特にビーム
シフトが問題となる。そこで、副アンテナを設置するた
めに主アンテナの主反射鏡面に設けた穴と同じ大きさの
穴を、主反射鏡上の対称な位置に設けることにより、ま
た副アンテナを設置するために主アンテナの主反射鏡面
に設けた穴に、周波数選択鏡面を設けることにより、こ
の問題を解決している。
In the antenna device of the present invention, since the sub-antenna for capturing is installed in the surface of the main reflecting mirror of the main antenna on the side opposite to the radio wave emission direction, it is necessary to make a hole in the main reflecting mirror surface. The main antenna causes beam shift and gain reduction, but beam shift becomes a problem especially in rocket tracking radar. Therefore, by installing holes of the same size as the holes provided on the main reflecting mirror surface of the main antenna for installing the sub-antenna at symmetrical positions on the main reflecting mirror, the main antenna for installing the sub-antenna again. This problem is solved by providing a frequency selective mirror surface in the hole provided in the main reflective mirror surface.

【0011】[0011]

【実施例】以下、この発明の一実施例を図について説明
する。図1はこの発明の第1の実施例によるアンテナ装
置を示す。図において、1は主アンテナ、1aはそのホ
ーン、2はこの主アンテナ21の内側に設置した捕捉用
副アンテナ、2aはそのホーン、3は主アンテナの主反
射鏡、11は捕捉用副アンテナを設置するために主アン
テナ1の主反射鏡3に設けた穴、12は主アンテナ1の
主反射鏡3上に穴11と対称な位置にこれと同じ大きさ
で設けた穴である。
DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described below with reference to the drawings. FIG. 1 shows an antenna device according to a first embodiment of the present invention. In the figure, 1 is a main antenna, 1a is its horn, 2 is a capturing sub-antenna installed inside this main antenna 21, 2a is its horn, 3 is a main reflecting mirror of the main antenna, and 11 is a capturing sub-antenna. A hole 12 is provided on the main reflecting mirror 3 of the main antenna 1 for installation, and a hole 12 is provided on the main reflecting mirror 3 of the main antenna 1 at a position symmetrical to the hole 11 and of the same size.

【0012】次に作用,効果について説明する。主アン
テナ1の主反射鏡3に穴11を設ける場合、主アンテナ
1はビームシフト及び利得低下が生じる。
Next, the operation and effect will be described. When the hole 11 is provided in the main reflecting mirror 3 of the main antenna 1, the main antenna 1 undergoes beam shift and gain reduction.

【0013】例えば、直径7mの主アンテナ内に直径
0.4mの捕捉用副アンテナを設置するため主反射鏡の
中心から半径2mの位置に直径0.4mの穴を設けた場
合、周波数6GHzにおいて、ビームシフト約0.00
14°,利得低下約0.03dB(計算値)が生じる。
For example, when a 0.4 m diameter capturing sub-antenna is installed in a 7 m diameter main antenna and a 0.4 m diameter hole is provided at a radius of 2 m from the center of the main reflecting mirror, the frequency is 6 GHz. , Beam shift about 0.00
At 14 °, a gain decrease of about 0.03 dB (calculated value) occurs.

【0014】ところで、ロケットを追尾するレーダに適
用するアンテナ装置の場合、特にこのビームシフトが測
角精度の低下を招き、問題となる。
By the way, in the case of an antenna device applied to a radar for tracking a rocket, this beam shift causes a problem in that the angle measurement accuracy is deteriorated.

【0015】このビームシフトは主反射鏡上に穴を設け
ることにより、主反射鏡上で非対称な位相誤差が生じる
ため発生するものである。しかしながら、主反射鏡上の
対称な位置に同じ大きさの穴を設ければ、位相誤差の非
対称性がなくなり、もはやビームシフトは生じない。
This beam shift occurs because an asymmetrical phase error is generated on the main reflecting mirror by providing a hole on the main reflecting mirror. However, if holes of the same size are provided at symmetrical positions on the main reflecting mirror, the asymmetry of the phase error is eliminated and the beam shift no longer occurs.

【0016】なお、この場合の利得低下を計算すれば、
その値は約0.06dBとなり、これは特に問題とはな
らない値である。
If the gain reduction in this case is calculated,
The value is about 0.06 dB, which is not a particular problem.

【0017】なお、上記実施例は主反射鏡上に捕捉用副
アンテナを設置するために設けた穴と点対称な位置に同
じ大きさの穴を設けるようにしたものを示したが、図2
に示す本発明の第2の実施例のように、捕捉用副アンテ
ナ2を設置するために設けた穴11に主アンテナ1の電
波22を反射し、捕捉用副アンテナ2の電波23を透過
する周波数選択鏡面(FSR:Frequency Selective Re
flector)21を設けるようにすればよい。この場合、上
記実施例のように主反射鏡上の対称な位置に同じ大きさ
の穴を設ける必要はなく、加工に要する手間が少なくて
済み、加工に伴う主反射鏡面の変形を最小限に抑えるこ
とができるという効果がある。
In the above embodiment, a hole of the same size is provided on the main reflecting mirror at a position point-symmetrical to the hole provided for installing the sub-antenna for capturing.
As in the second embodiment of the present invention shown in FIG. 2, the radio wave 22 of the main antenna 1 is reflected in the hole 11 provided for installing the sub-antenna 2 for capturing, and the radio wave 23 of the sub-antenna 2 for capturing is transmitted. Frequency selective mirror surface (FSR: Frequency Selective Re
a flector) 21 may be provided. In this case, it is not necessary to provide holes of the same size at symmetrical positions on the main reflecting mirror as in the above embodiment, the labor required for processing is small, and the deformation of the main reflecting mirror surface due to processing is minimized. The effect is that it can be suppressed.

【0018】[0018]

【発明の効果】以上のように、この発明に係るアンテナ
装置によれば、主アンテナの内側に、主アンテナに比較
して指向性ならびに利得が小さい副アンテナを設置し、
かつ副アンテナを設置するために設けた主アンテナの主
反射鏡上の穴と主反射鏡上の対称な位置に同じ大きさの
穴を設けるようにしたので、捕捉用副アンテナを主アン
テナと別に設置する場合に比べ安価にでき、また自重変
形による影響が小さいため、測角精度の高いアンテナ装
置が得られる効果がある。
As described above, according to the antenna device of the present invention, the sub-antenna having the directivity and the gain smaller than that of the main antenna is installed inside the main antenna,
In addition, since the holes on the main reflecting mirror of the main antenna provided to install the sub antenna and the holes of the same size are provided at symmetrical positions on the main reflecting mirror, the capturing sub antenna is separated from the main antenna. Since it is cheaper than the case where it is installed and the influence of its own weight deformation is small, there is an effect that an antenna device with high angle measurement accuracy can be obtained.

【0019】また、主アンテナの内側に、主アンテナに
比較して指向性ならびに利得が小さい副アンテナを設置
し、かつ副アンテナを設置するために設けた主アンテナ
の主反射鏡上の穴に周波数選択鏡面を設けるようにした
ので、主アンテナの主反射鏡に穴を1つ設けるだけで済
み、かつ捕捉用副アンテナを主アンテナと別に設置する
場合に比べ安価にでき、また自重変形による影響が小さ
いため、測角精度の高いアンテナ装置が得られる効果が
ある。
Further, a sub-antenna having a directivity and a gain smaller than that of the main antenna is installed inside the main antenna, and a frequency is provided in a hole on the main reflecting mirror of the main antenna provided for installing the sub-antenna. Since the selective mirror surface is provided, it is only necessary to provide one hole in the main reflecting mirror of the main antenna, and the cost can be reduced as compared with the case where the capturing sub-antenna is installed separately from the main antenna. Since it is small, there is an effect that an antenna device with high angle measurement accuracy can be obtained.

【図面の簡単な説明】[Brief description of drawings]

【図1】この発明の第1の実施例によるアンテナ装置を
示す断面側面図および平面図である。
FIG. 1 is a sectional side view and a plan view showing an antenna device according to a first embodiment of the present invention.

【図2】この発明の第2の実施例によるアンテナ装置を
示す断面側面図である。
FIG. 2 is a sectional side view showing an antenna device according to a second embodiment of the present invention.

【図3】従来のアンテナ装置を示す平面図である。FIG. 3 is a plan view showing a conventional antenna device.

【符号の説明】[Explanation of symbols]

1 主アンテナ 2 副アンテナ 3 主アンテナの主反射鏡 11 主アンテナの主反射鏡上に設けた穴 12 主アンテナの主反射鏡上に設けた穴11と対称な
位置に同じ大きさで設けた穴 21 周波数選択鏡面(FSR) 22 主アンテナの電波 23 副アンテナの電波
1 main antenna 2 sub-antenna 3 main reflecting mirror of main antenna 11 hole provided on the main reflecting mirror of the main antenna 12 hole provided on the main reflecting mirror of the main antenna at a position symmetrical to the hole 11 having the same size 21 Frequency Selective Mirror (FSR) 22 Radio wave from main antenna 23 Radio wave from sub antenna

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 指向性の大きい主アンテナの電波放射方
向と反対側に、主アンテナに比較して指向性ならびに利
得が小さい副アンテナを設置し、 副アンテナを設置するために設けた主アンテナの主反射
鏡上の穴と主反射鏡上の中心に関し点対称な位置に同じ
大きさの穴を設けてなることを特徴とするアンテナ装
置。
1. A sub-antenna having a directivity and a gain smaller than that of the main antenna is installed on the side opposite to the radio wave radiation direction of the main antenna having a large directivity, and the main antenna provided for installing the sub-antenna An antenna device comprising a hole on the main reflecting mirror and a hole of the same size provided at points symmetrical with respect to the center of the main reflecting mirror.
【請求項2】 指向性の大きい主アンテナの電波放射方
向と反対側に、主アンテナに比較して指向性ならびに利
得が小さい副アンテナを設置し、 副アンテナを設置するために設けた主アンテナの主反射
鏡上の穴に周波数選択鏡面を設けてなることを特徴とす
るアンテナ装置。
2. A sub-antenna having a directivity and a gain smaller than that of the main antenna is installed on the side opposite to the radio wave radiating direction of the main antenna having a large directivity, and the main antenna provided to install the sub-antenna. An antenna device characterized in that a frequency selective mirror surface is provided in a hole on a main reflecting mirror.
JP19261891A 1991-07-05 1991-07-05 Antenna system Pending JPH0514050A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19261891A JPH0514050A (en) 1991-07-05 1991-07-05 Antenna system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19261891A JPH0514050A (en) 1991-07-05 1991-07-05 Antenna system

Publications (1)

Publication Number Publication Date
JPH0514050A true JPH0514050A (en) 1993-01-22

Family

ID=16294259

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19261891A Pending JPH0514050A (en) 1991-07-05 1991-07-05 Antenna system

Country Status (1)

Country Link
JP (1) JPH0514050A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8496251B2 (en) 2010-01-12 2013-07-30 Nok Corporation Sealing system
JP6022139B1 (en) * 2016-04-08 2016-11-09 三菱電機株式会社 RESONANT ELEMENT OF FREQUENCY SELECTION PLATE, FREQUENCY SELECTION PLATE AND ANTENNA DEVICE

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8496251B2 (en) 2010-01-12 2013-07-30 Nok Corporation Sealing system
US8608177B2 (en) 2010-01-12 2013-12-17 Nok Corporation Sealing system
JP6022139B1 (en) * 2016-04-08 2016-11-09 三菱電機株式会社 RESONANT ELEMENT OF FREQUENCY SELECTION PLATE, FREQUENCY SELECTION PLATE AND ANTENNA DEVICE
WO2017175386A1 (en) * 2016-04-08 2017-10-12 三菱電機株式会社 Resonant element for frequency selective plate, frequency selective plate and antenna device
US10938118B2 (en) 2016-04-08 2021-03-02 Mitsubishi Electric Corporation Resonant element of frequency selective surface, frequency selective surface and antenna device

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