JPH033502A - Mirror surface correction antenna - Google Patents

Mirror surface correction antenna

Info

Publication number
JPH033502A
JPH033502A JP13785489A JP13785489A JPH033502A JP H033502 A JPH033502 A JP H033502A JP 13785489 A JP13785489 A JP 13785489A JP 13785489 A JP13785489 A JP 13785489A JP H033502 A JPH033502 A JP H033502A
Authority
JP
Japan
Prior art keywords
antenna
error signal
reception
reflector
detection section
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
Application number
JP13785489A
Other languages
Japanese (ja)
Other versions
JP3005229B2 (en
Inventor
Yoshihide Miyata
宮田 吉秀
Satoshi Miyatani
宮谷 聡
Tomoki Kobuchi
知己 小渕
Noboru Toyama
昇 外山
Kenji Oumaru
王丸 謙治
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.)
NEC Corp
Japan Broadcasting Corp
Original Assignee
NEC Corp
Nippon Hoso Kyokai NHK
Japan Broadcasting 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 NEC Corp, Nippon Hoso Kyokai NHK, Japan Broadcasting Corp filed Critical NEC Corp
Priority to JP1137854A priority Critical patent/JP3005229B2/en
Publication of JPH033502A publication Critical patent/JPH033502A/en
Application granted granted Critical
Publication of JP3005229B2 publication Critical patent/JP3005229B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Aerials With Secondary Devices (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

PURPOSE:To attain tracking and reception, to reduce the weight and to avoid a limit of mounted location without separate use of a tracking reception antenna by combining an error signal detection section to a mirror surface correction antenna. CONSTITUTION:A reception signal (17GHz) received by a mirror surface correction antenna 1 in common use of a transmission reception antenna and a tracking reception antenna for receiving broadcast is inputted to an error signal detection section 2 via a feeding horn 13, the beam width is selected and outputted as an error signal. A processing system 4 applies direction control of the antenna 1 based on an error signal extracted by an error signal detection section 2. On the other hand, a repeater system 3 converts an error signal of the error signal detection section 2 into a 12GHz broadcast signal, it is relayed to the error signal detection section 2 and radiates from the antenna 1 onto ground. Thus, the error signal detection section 2 selects the beam width at the transmission frequency band and the reception frequency band and the correction of the reflecting mirror to eliminate the use for the antenna for exclusive use of tracking and reception and the weight is reduced.

Description

【発明の詳細な説明】 【産業上の利用分野] 本発明は複反射鏡アンテナの鏡面を修整して電波の進行
方向に直角な断面におけるビーム形状が高度な成形ビー
ムを得る鏡面修整アンテナに関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a mirror-modified antenna that obtains a shaped beam with a high degree of beam shape in a cross section perpendicular to the direction of propagation of radio waves by modifying the mirror surface of a double-reflector antenna.

〔従来の技術〕[Conventional technology]

従来、複反射鏡アンテナで高度な成形ビームを得る方法
として鏡面修整オフセットグレゴリアンアンテナ等が考
案されている(昭和63年電子情報通信学会春季全国大
会5B−1−2r鏡面修整による高度成形ビームアンテ
ナ」正源、王丸、 NHK)。この鏡面修整アンテナを
使用して人工衛星から12GHz帯の周波数で放送サー
ビスを行う場合、常に一定方向にアンテナを指向させる
ために、17GHz帯の地上局からの信号を使い指向誤
差を検出するためのアンテナが別に必要であった。
Conventionally, as a method of obtaining a highly shaped beam using a double-reflector antenna, a mirror-modified offset Gregorian antenna has been devised (1986 Institute of Electronics, Information and Communication Engineers Spring National Conference 5B-1-2r Advanced Shaped Beam Antenna by Mirror Modification). Shogen, Oumaru, NHK). When using this mirror-finished antenna to provide broadcasting services from an artificial satellite at a frequency in the 12 GHz band, in order to always point the antenna in a fixed direction, a signal from a ground station in the 17 GHz band is used to detect pointing errors. A separate antenna was required.

従来例を第2図に示す。lは主反射鏡11及び副反射鏡
12並びに給電ホーン13からなる複反射鏡型鏡面修整
アンテナ、32は中継器、41は追尾受信機(TRCK
 −RCVR)、42はアンテナ指向制御回路、43は
アンテナ指向制御機構(APM) 、5は受信用アンテ
す、51は受信用アンテナ5の反射鏡、52は受信用ア
ンテナ5の給電ホーンであり、これらの機器は人工衛星
の本体6に搭載されている。受信用アンテナ5で受信さ
れ給電ホーン52から出力された17GHz帯の受信信
号は中継器32で12GHz帯送信周波数に変換されて
鏡面修整アンテナ1より地球に向けて放射される。
A conventional example is shown in FIG. 1 is a double-reflector type mirror-finished antenna consisting of a main reflector 11, a sub-reflector 12, and a feeding horn 13; 32 is a repeater; 41 is a tracking receiver (TRCK);
-RCVR), 42 is an antenna pointing control circuit, 43 is an antenna pointing control mechanism (APM), 5 is a receiving antenna, 51 is a reflector of the receiving antenna 5, 52 is a feeding horn of the receiving antenna 5, These devices are mounted on the main body 6 of the artificial satellite. A 17 GHz band reception signal received by the reception antenna 5 and output from the feeding horn 52 is converted into a 12 GHz band transmission frequency by the repeater 32 and radiated toward the earth from the mirror-finished antenna 1.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

上述した従来の鏡面修整アンテナ1は12G)Iz送信
周波数帯で高度な成形ビームが得られるように副反射鏡
12を凹凸させて主反射鏡11面上の振幅分布及び主反
射鏡面を凹凸させて主反射鏡開口面上の位相分布を修整
しているため、この鏡面修整アンテナ1を使用し、17
GHz帯の受信信号を使用して追尾を行う場合、別のア
ンテナで指向させる方向を検出し、このデータを基に鏡
面修整アンテナ1を指向させるという追尾方式が提案さ
れている。
The above-mentioned conventional mirror-finished antenna 1 has a sub-reflector 12 made uneven to make the amplitude distribution on the surface of the main reflector 11 and the main reflecting mirror surface uneven so that a highly shaped beam can be obtained in the 12G) Iz transmission frequency band. Since the phase distribution on the main reflector aperture is modified, this mirror-finished antenna 1 is used, and 17
When tracking is performed using a received signal in the GHz band, a tracking method has been proposed in which the direction in which another antenna is directed is detected, and the mirror surface modification antenna 1 is directed based on this data.

特に、人工衛星に従来の鏡面修整アンテナを搭載する場
合、追尾用として鏡面修整アンテナ1とは別に追尾及び
受信専用のアンテナ5が必要となり、重量増加等の欠点
がある。
In particular, when a conventional mirror-finished antenna is mounted on an artificial satellite, an antenna 5 dedicated to tracking and reception is required in addition to the mirror-finished antenna 1 for tracking, which has drawbacks such as increased weight.

本発明の目的は前記課題を解決した通信装置を提供する
ことにある。
An object of the present invention is to provide a communication device that solves the above problems.

〔課題を解決するための手段〕[Means to solve the problem]

前記目的を達成するため、本発明は電波の進行方向に直
角な断面におけるアンテナ放射パターンの形状を、高度
な成形ビームとなるように副反射鏡を凹凸させて主反射
鏡面上の振幅分布及び主反射鏡面を凹凸させて主反射鏡
開口面上の位相分布を修整する複反射鏡型の鏡面修整ア
ンテナにおいて、前記複反射鏡型鏡面修整アンテナを放
送信号の送受信用アンテナ及び追尾受信用アンテナに兼
用し、さらに複反射鏡型鏡面修整アンテナの給電ホーン
の送信周波数帯及び受信周波数帯のビーム幅、反射鏡の
修整量を適切に選択することにより、送信周波数帯では
高度な成形ビームを得、かつ受信周波数帯では良好な誤
差信号を得る誤差信号検出部を有するものである。
In order to achieve the above object, the present invention improves the shape of the antenna radiation pattern in a cross section perpendicular to the direction of propagation of radio waves by making the sub-reflector uneven so that it becomes a highly shaped beam, thereby changing the amplitude distribution on the main reflecting mirror surface and the main beam. In a double-reflector-type mirror-finished antenna that modifies the phase distribution on the main reflector aperture by making the reflecting mirror surface uneven, the double-reflector-type mirror-finished antenna is used both as a broadcast signal transmission/reception antenna and as a tracking reception antenna. Furthermore, by appropriately selecting the beam width of the transmitting frequency band and the receiving frequency band of the feed horn of the double-reflector mirror-finished antenna, and the amount of modification of the reflector, a highly shaped beam can be obtained in the transmitting frequency band. It has an error signal detection section that obtains a good error signal in the reception frequency band.

〔実施例〕〔Example〕

以下、本発明の一実施例を図により説明する。 Hereinafter, one embodiment of the present invention will be described with reference to the drawings.

第1図は本発明の一実施例を示す構成図である。FIG. 1 is a block diagram showing an embodiment of the present invention.

図において、1は主反射鏡11及び副反射鏡12並びに
給電ホーン13からなり、人工衛星本体6に搭載される
複反射鏡型鏡面修整アンテナであり、該鏡面修整アンテ
ナlは電波の進行方向に直角な断面におけるアンテナ放
射パターンの形状を、高度な成形ビームとなるように副
反射鏡12を凹凸させて主反射鏡11の面上での振幅分
布及び主反射鏡面を凹凸させて主反射鏡開口面上の位相
分布を修整する構造になっている。前記高度な成形ビー
ムは例えば日本列島の形状に合った成形ビームに整形さ
れる。
In the figure, reference numeral 1 denotes a double-reflector-type mirror-finished antenna that includes a main reflector 11, a sub-reflector 12, and a feeding horn 13, and is mounted on the satellite body 6. The mirror-finished antenna 1 is arranged in the direction of propagation of radio waves. The shape of the antenna radiation pattern in a right-angled cross section is changed by making the sub-reflector 12 uneven and the amplitude distribution on the surface of the main reflecting mirror 11 and the main reflecting mirror aperture by making the main reflecting mirror surface uneven so that it becomes a highly shaped beam. It has a structure that modifies the phase distribution on the surface. The highly shaped beam is shaped into a shaped beam that matches the shape of the Japanese archipelago, for example.

本発明は前記複反射鏡型鏡面修整アンテナ1を放送信号
の送受信用アンテナ及び追尾受信用アンテナに兼用し、
さらに、鏡面修整アンテナ1の給電ホーン13の送信周
波数(12Gl(zの放送信号)帯及び受信周波数(地
上局からの17GHzの受信信号)帯のビーム幅、反射
鏡11.12の修整量を選択する誤差信号検出部2と、
誤差信号検出部2にて得られた誤差信号(17GHz)
に基づいて鏡面修整アンテナ11特に副反射鏡12の指
向制御を行う処理系4と、誤差信号検出部2よりの誤差
信号を放送信号(12GHz)に変換して誤差信号検出
部2に中継する中継器系3とを有し、これらを人工衛星
本体6に搭載したものである。
The present invention uses the double-reflector type mirror-finished antenna 1 as an antenna for transmitting and receiving broadcast signals and as an antenna for tracking and receiving,
Furthermore, the beam width of the transmission frequency (12Gl (z broadcast signal) band and reception frequency (17GHz reception signal from the ground station) band of the feeding horn 13 of the mirror surface modification antenna 1 and the amount of modification of the reflector 11 and 12 are selected. an error signal detection unit 2,
Error signal obtained by error signal detection section 2 (17 GHz)
a processing system 4 that performs directivity control of the mirror surface modification antenna 11, particularly the sub-reflector 12, based on The artificial satellite body 6 has an organ system 3 and these are mounted on the artificial satellite main body 6.

前記誤差信号検出部2は追尾用の誤差信号を検出する方
式として、マルチホーン方式又は高次モード方式のいず
れを用いてもよい。
The error signal detection section 2 may use either a multi-horn method or a high-order mode method as a method for detecting an error signal for tracking.

中継器系3はダイプレクサ(D I P)31、中継器
32を含み、受信された17GHzの受信信号を12G
Hz帯の放送信号に変換する。
The repeater system 3 includes a diplexer (DIP) 31 and a repeater 32, and converts the received 17GHz signal to 12G.
Convert to Hz band broadcast signal.

処理系4は追尾する受信機(TRCK −RCVR)4
1 、アンテナ指向制御回路(APE) 42、アンテ
ナ指向機構(APM) 43を含む。
The processing system 4 is a tracking receiver (TRCK-RCVR) 4
1, an antenna pointing control circuit (APE) 42, and an antenna pointing mechanism (APM) 43.

実施例において、鏡面修整アンテナ1にて受信された受
信信号(17GHz)は給電ホーン13を介して誤差信
号検出部2に入力し、そのビーム幅が選択され、誤差信
号として出力される。
In the embodiment, a received signal (17 GHz) received by the mirror-finished antenna 1 is input to the error signal detection unit 2 via the feeding horn 13, its beam width is selected, and the signal is output as an error signal.

誤差信号検出部2で取り出された誤差信号に基づいて処
理系4はアンテナ1の指向制御を行う。
A processing system 4 performs directivity control of the antenna 1 based on the error signal extracted by the error signal detection section 2.

一方、中継器系3は誤差信号検出部2の誤差信号を12
GHzの放送信号に変換し、これが誤差信号検出部2に
中継され、アンテナ1から地上に向けて放射される。
On the other hand, the repeater system 3 converts the error signal of the error signal detection section 2 into 12
It is converted into a GHz broadcast signal, which is relayed to the error signal detection section 2 and radiated from the antenna 1 toward the ground.

以上のように、誤差信号検出部2は送信周波数帯及び受
信周波数帯におけるビーム幅、反射鏡の修整量を選択す
ることにより、送信周波数帯では高度な成形ビームを得
、かつ受信周波数帯で良好な誤差信号を得ることになる
As described above, the error signal detection unit 2 obtains a highly shaped beam in the transmission frequency band and a well-shaped beam in the reception frequency band by selecting the beam width and the amount of modification of the reflector in the transmission frequency band and the reception frequency band. This results in an accurate error signal.

[発明の効果] 以上説明したように本発明は、鏡面修整アンテナに誤差
信号検出部を組合せることにより、追尾受信用アンテナ
を別に用いず追尾及び送・受信でき、重量軽減及び搭載
場所の制限を減らす効果がある。さらに、鏡面修整アン
テナで誤差信号を検出しているため、アンテナの指向精
度も高いという効果がある。
[Effects of the Invention] As explained above, the present invention combines a mirror-finished antenna with an error signal detection section to enable tracking, transmission and reception without using a separate tracking and receiving antenna, reducing weight and limiting the mounting location. It has the effect of reducing Furthermore, since the error signal is detected using a mirror-finished antenna, the antenna has a high pointing accuracy.

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

第1図は本発明の一実施例を示す構成図、第2図は従来
例を示す構成図である。 2・・・誤差信号検出部 4・・・処理系 l・・・鏡面修整アンテナ 3・・・中継器系 6・・・人工衛星本体
FIG. 1 is a block diagram showing an embodiment of the present invention, and FIG. 2 is a block diagram showing a conventional example. 2...Error signal detection unit 4...Processing system l...Mirror surface modification antenna 3...Relay system 6...Satellite main body

Claims (1)

【特許請求の範囲】[Claims] (1)電波の進行方向に直角な断面におけるアンテナ放
射パターンの形状を、高度な成形ビームとなるように副
反射鏡を凹凸させて主反射鏡面上の振幅分布及び主反射
鏡面を凹凸させて主反射鏡開口面上の位相分布を修整す
る複反射鏡型の鏡面修整アンテナにおいて、前記複反射
鏡型鏡面修整アンテナを放送信号の送受信用アンテナ及
び追尾受信用アンテナに兼用し、さらに複反射鏡型鏡面
修整アンテナの給電ホーンの送信周波数帯及び受信周波
数帯のビーム幅、反射鏡の修整量を適切に選択すること
により、送信周波数帯では高度な成形ビームを得、かつ
受信周波数帯では良好な誤差信号を得る誤差信号検出部
とを有することを特徴とする鏡面修整アンテナ。
(1) The shape of the antenna radiation pattern in a cross section perpendicular to the direction of radio wave propagation is changed by making the sub-reflector uneven and the amplitude distribution on the main reflecting mirror surface and the main reflecting mirror surface uneven so that it becomes a highly shaped beam. In a double-reflector-type mirror-finishing antenna that modifies the phase distribution on the reflector aperture, the double-reflector-type mirror-finish antenna is used both as a transmitting and receiving antenna for broadcasting signals and as a tracking reception antenna. By appropriately selecting the beam width in the transmission frequency band and reception frequency band of the feeding horn of the mirror-modified antenna, and the modification amount of the reflector, a highly shaped beam can be obtained in the transmission frequency band, and a good error error can be achieved in the reception frequency band. 1. A mirror surface modified antenna, comprising: an error signal detection section for obtaining a signal.
JP1137854A 1989-05-31 1989-05-31 Mirror modified antenna Expired - Lifetime JP3005229B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1137854A JP3005229B2 (en) 1989-05-31 1989-05-31 Mirror modified antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1137854A JP3005229B2 (en) 1989-05-31 1989-05-31 Mirror modified antenna

Publications (2)

Publication Number Publication Date
JPH033502A true JPH033502A (en) 1991-01-09
JP3005229B2 JP3005229B2 (en) 2000-01-31

Family

ID=15208337

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1137854A Expired - Lifetime JP3005229B2 (en) 1989-05-31 1989-05-31 Mirror modified antenna

Country Status (1)

Country Link
JP (1) JP3005229B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPWO2014061293A1 (en) * 2012-10-16 2016-09-05 三菱電機株式会社 Reflector antenna device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPWO2014061293A1 (en) * 2012-10-16 2016-09-05 三菱電機株式会社 Reflector antenna device
US9543659B2 (en) 2012-10-16 2017-01-10 Mitsubishi Electric Corporation Reflector antenna device

Also Published As

Publication number Publication date
JP3005229B2 (en) 2000-01-31

Similar Documents

Publication Publication Date Title
KR100887043B1 (en) Low cost high performance antenna for use in interactive satellite terminals
RU2163052C2 (en) Device and method for signal transmission and reception using adaptive antenna
US7957425B2 (en) Communicating distinct data using polarized data signals
US3836970A (en) Antenna array for aircraft navigation system
HU221392B1 (en) Method and arrangement for the telecommunication by electromagnetic waves
USH1383H (en) Space-based tethered phased-array antenna
US7154439B2 (en) Communication satellite cellular coverage pointing correction using uplink beacon signal
US20020077153A1 (en) Mobile communication system and communication method performed in the system
JPH033502A (en) Mirror surface correction antenna
US20070060046A1 (en) Apparatus for repeating signal using microstrip patch array antenna
JPH09326630A (en) Adaptive array antenna system
JPH08146119A (en) Radar device
JP6431775B2 (en) Phase detector and satellite repeater
Adams Beam tagging for control of adaptive transmitting arrays
JP3588965B2 (en) Adaptive receiver
JPS60228981A (en) Radar equipment
JPH041522B2 (en)
JPH01233381A (en) Radar
JP3275959B2 (en) Antenna system
JP2002232335A (en) System and equipment for receiving diversity satellite broadcasting
JPH11205213A (en) Transmitter-receiver for space vehicle
JPS5827467B2 (en) direction finding method
JP2000059128A (en) Diversity antenna
KR20010063792A (en) Active phased array antenna system and beam control method for mobile satellite communications
JPH01142478A (en) Secondary radiation suppression circuit by side band antenna