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JPH05336012A - Satellite-mounted repeater - Google Patents

Satellite-mounted repeater

Info

Publication number
JPH05336012A
JPH05336012A JP13855392A JP13855392A JPH05336012A JP H05336012 A JPH05336012 A JP H05336012A JP 13855392 A JP13855392 A JP 13855392A JP 13855392 A JP13855392 A JP 13855392A JP H05336012 A JPH05336012 A JP H05336012A
Authority
JP
Japan
Prior art keywords
frequency
oscillator
satellite
beacon
reference oscillator
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
JP13855392A
Other languages
Japanese (ja)
Inventor
Kazuichi Yamamoto
員市 山本
Masayoshi Tanaka
將義 田中
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.)
Nippon Telegraph and Telephone Corp
Original Assignee
Nippon Telegraph and Telephone 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 Nippon Telegraph and Telephone Corp filed Critical Nippon Telegraph and Telephone Corp
Priority to JP13855392A priority Critical patent/JPH05336012A/en
Publication of JPH05336012A publication Critical patent/JPH05336012A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To make a frequency highly stable while keeping communication by making the local oscillator of a frequency converter and a beacon oscillator synchronize with a common reference oscillator and providing a frequency adjusting function on the reference oscillator. CONSTITUTION:This satellite-mounted repeater generates a local oscillating frequency used for frequency converters 6-1-6-n converting the frequency into an up-link frequency and a down-link frequency and the beacon frequency of the beacon oscillator 8 by using a common original frequency generated from a reference oscillator 9 whose oscillating frequency is variable. Thus, the frequency stability of the satellite-mounted repeater depends only on the frequency stability of the reference oscillator 9. When the frequency of the reference oscillator is fluctuated, the high stability of the frequency of the satellite-mounted repeater is realized by adjusting the frequency of the reference oscillator so as to eliminate the fluctuation. Furthermore, the frequency is adjusted while keeping the communication.

Description

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

【0001】[0001]

【産業上の利用分野】本発明は衛星搭載中継器に関する
もので、特に、周波数安定度の高い衛星搭載中継器に係
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a satellite-mounted repeater, and more particularly to a satellite-mounted repeater having high frequency stability.

【0002】[0002]

【従来の技術】図4に従来の衛星搭載中継器のビーコン
および周波数変換に関する主要部分の構成の例を示す。
この図において、1-1〜1-n+1は基準発振器、6-1〜6
-nは周波数変換器、2-1〜2-nは周波数変換器の局部発
振系、3-1〜3-nは周波数変換器のミキサ、4-1〜4-n
は周波数変換器のRF系入力部、5-1〜5-nは周波数変
換器のRF系出力部、7はビーコン周波数生成系、8は
ビーコン発振器を表わしている。
2. Description of the Related Art FIG. 4 shows an example of the configuration of a main part of a conventional satellite-mounted repeater related to beacons and frequency conversion.
In this figure, 1 -1 to 1 -n + 1 are reference oscillators, 6 -1 to 6
-n is a frequency converter, 2 -1 to 2 -n is a local oscillation system of the frequency converter, 3 -1 to 3 -n is a mixer of the frequency converter, 4 -1 to 4 -n
Is an RF input unit of the frequency converter, 5 -1 to 5- n is an RF output unit of the frequency converter, 7 is a beacon frequency generation system, and 8 is a beacon oscillator.

【0003】従来、この種の周波数変動が小さい衛星搭
載中継器は、図4に示すように周波数安定度が非常に高
い水晶発振器等の個別の基準発振器1-1〜1-nにより原
振周波数を供給し、局部発振系2-1〜2-nにより、アッ
プリンク周波数をダウンリンク周波数に変換する周波数
変換器6-1〜6-nに使用する局部発振周波数を生成する
構成を採っていた。また、ビーコン発振器8についても
独立の基準発振器1-n +1による原振周波数からビーコン
周波数を生成する構成を採っていた。
Conventionally, this kind of satellite-mounted repeater with a small frequency fluctuation has an original oscillation frequency by an individual reference oscillator 1 -1 to 1 -n such as a crystal oscillator having a very high frequency stability as shown in FIG. supplying, by a local oscillation system 2 -1 to 2 -n, it was adopted a structure that generates a local oscillation frequency used in the frequency converter 6 -1 to 6 -n for converting the uplink frequency to the downlink frequency .. The beacon oscillator 8 also has a configuration in which the beacon frequency is generated from the original oscillation frequency by the independent reference oscillator 1 -n +1 .

【0004】[0004]

【発明が解決しようとする課題】従来の周波数変動が小
さい衛星搭載中継器は上述のように構成されるので、周
波数安定度は局部発振系の原振周波数を供給する水晶発
振器等の個別の基準発振器1-1〜1-nの周波数安定度に
依存していた。このため、複数個ある周波数変換器の周
波数は、各々独立に変動すること、各基準発振器の原振
周波数が変化した場合に何ら調整する機能が存在しない
こと、および、周波数変動を検知するためには衛星搭載
中継器に無変調信号を入力し、その出力無変調信号の周
波数を測定しなければならず、そのため、周波数変動の
測定のために通信サービスを中断しなければならないと
言う欠点があった。
Since the conventional satellite-mounted repeater with a small frequency fluctuation is constructed as described above, the frequency stability is determined by an individual reference such as a crystal oscillator for supplying the original oscillation frequency of the local oscillation system. It depended on the frequency stability of the oscillators 1 -1 to 1 -n . For this reason, the frequencies of a plurality of frequency converters vary independently, that there is no function to adjust when the original oscillator frequency of each reference oscillator changes, and to detect frequency fluctuations. Has to input an unmodulated signal into a satellite repeater and measure the frequency of its output unmodulated signal, which has the drawback that communication services must be interrupted to measure frequency fluctuations. It was

【0005】本発明は上記のような欠点を解決するため
になされたもので、周波数の調整機能を付加することで
局部発振系の原振周波数を供給する基準発振器の性能に
依存せずに周波数安定度が高い衛星搭載中継器を実現す
ると共に、通信を継続したまま周波数変動の検出、およ
び周波数の調整が可能な衛星搭載中継器を実現すること
を目的とする。
The present invention has been made to solve the above-mentioned drawbacks, and by adding a frequency adjusting function, the frequency can be obtained without depending on the performance of the reference oscillator that supplies the original oscillation frequency of the local oscillation system. It is an object of the present invention to realize a satellite-mounted repeater with high stability and to realize a satellite-mounted repeater capable of detecting frequency fluctuations and adjusting frequencies while continuing communication.

【0006】[0006]

【課題を解決するための手段】図1は本発明の原理的構
成を示す図であって、衛星搭載中継器のビーコンおよび
周波数変換に関する主要部分の構成を示している。この
図において、6-1〜6 -nは周波数変換器、2-1〜2-n
周波数変換器の局部発振系、3-1〜3-nは周波数変換器
のミキサ、4-1〜4-nは周波数変換器のRF系入力部、
-1〜5-nは周波数変換器のRF系出力部、7はビーコ
ン周波数生成系、8はビーコン発振器、9は周波数可変
の基準発振器、13は基準発振器の周波数制御手段を表
わしている。
FIG. 1 shows the principle structure of the present invention.
FIG. 3 is a diagram showing the configuration of the satellite repeater beacon and
The structure of the main part regarding frequency conversion is shown. this
In the figure, 6-1~ 6 -nIs a frequency converter, 2-1~ 2-nIs
Local oscillation system of frequency converter, 3-1~ 3-nIs a frequency converter
Mixer, 4-1~ 4-nIs the RF input part of the frequency converter,
5-1~ 5-nIs the RF output of the frequency converter, and 7 is Beco
Frequency generation system, 8 is a beacon oscillator, 9 is variable frequency
Reference oscillator, 13 is a frequency control means of the reference oscillator.
I forgot.

【0007】本発明の衛星搭載中継器は、図1に示すよ
うにアップリンク周波数をダウンリンク周波数に変換す
る周波数変換器6-1〜6-n、ビーコン発振器8、該周波
数変換器に使用する局部発振周波数および該ビーコン発
振器のビーコン周波数を生成するための共通の原振周波
数を供給する周波数可変の基準発振器9を備える。上記
基準発振器の原振周波数は各周波数変換器6-1〜6-n
局部発振周波数およびビーコン周波数の最大公約数を生
成するのに必要な周波数とする。
As shown in FIG. 1, the satellite-mounted repeater of the present invention is used for frequency converters 6 -1 to 6 -n for converting an uplink frequency into a downlink frequency, a beacon oscillator 8 and the frequency converter. A frequency-variable reference oscillator 9 is provided which supplies a local oscillation frequency and a common source frequency for generating the beacon frequency of the beacon oscillator. The original oscillation frequency of the reference oscillator is a frequency required to generate the greatest common divisor of the local oscillation frequency and the beacon frequency of each of the frequency converters 6 -1 to 6 -n .

【0008】[0008]

【作用】本発明の衛星搭載中継器は、図1の、アップリ
ンク周波数をダウンリンク周波数に変換する周波数変換
器6-1〜6-nに使用する局部発振周波数およびビーコン
発振器8のビーコン周波数を周波数可変の基準発振器9
から供給される共通の原振周波数を用いて生成する。
The satellite-mounted repeater of the present invention uses the local oscillator frequency and the beacon frequency of the beacon oscillator 8 used in the frequency converters 6 -1 to 6 -n for converting the uplink frequency into the downlink frequency in FIG. Variable frequency reference oscillator 9
It is generated using a common source frequency supplied from.

【0009】従って、本発明の衛星搭載中継器の周波数
安定度は、基準発振器9の周波数安定度だけに依存す
る。基準発振器9は周波数可変であるので、衛星搭載中
継器の周波数が変動した場合に、その変動が無くなるよ
うに基準発振器の周波数を調整することで衛星搭載中継
器の周波数の高安定化が実現できる。また、周波数変動
の様子は無変調信号であるビーコンの周波数を測定する
ことでモニタできるので、周波数の変化を検出するため
に通信を停止する必要がなく、通信を継続したまま周波
数の調整が可能である。
Therefore, the frequency stability of the satellite repeater of the present invention depends only on the frequency stability of the reference oscillator 9. Since the reference oscillator 9 has a variable frequency, when the frequency of the satellite-mounted repeater fluctuates, the frequency of the satellite-mounted repeater can be highly stabilized by adjusting the frequency of the reference oscillator so that the fluctuation does not occur. .. In addition, the state of frequency fluctuations can be monitored by measuring the frequency of the beacon, which is an unmodulated signal, so there is no need to stop communication to detect changes in frequency, and the frequency can be adjusted while communication is continued. Is.

【0010】基準発振器の周波数の制御方法は以下のよ
うな方法がある。無変調信号であるビーコンの周波数を
測定することで周波数変動の様子をモニタする。ビーコ
ン周波数の偏差を検出する手段によりビーコン周波数の
規定の周波数からの偏差を検出し、基準発振器の発振周
波数を制御する制御手段を用いてその偏差が無くなるよ
うに基準発振器の発振周波数を制御する。また、地上で
ビーコン周波数を測定して規定の周波数からの偏差を検
出し、その偏差が無くなるように地上から基準発振器の
発振周波数をコマンド等により制御するように制御系を
構成することも可能である。
There are the following methods for controlling the frequency of the reference oscillator. The frequency fluctuation is monitored by measuring the frequency of the beacon, which is an unmodulated signal. The means for detecting the deviation of the beacon frequency detects the deviation of the beacon frequency from the specified frequency, and the control means for controlling the oscillation frequency of the reference oscillator controls the oscillation frequency of the reference oscillator so as to eliminate the deviation. It is also possible to configure the control system so that the beacon frequency is measured on the ground, the deviation from the specified frequency is detected, and the oscillation frequency of the reference oscillator is controlled from the ground by a command so that the deviation disappears. is there.

【0011】周波数可変の基準発振器9は、電圧制御発
振器(VCO)、電圧制御水晶発振器(VCXO)等を
用いて構成でき、その場合には、発振周波数を制御する
ためには電圧を制御するだけで良い。
The variable frequency reference oscillator 9 can be constructed by using a voltage controlled oscillator (VCO), a voltage controlled crystal oscillator (VCXO) or the like. In that case, in order to control the oscillation frequency, only the voltage is controlled. Good.

【0012】なお、複数の周波数変換器を用いてアップ
リンク周波数をダウンリンク周波数に周波数変換する構
成の場合には、各周波数変換器に使用する局部発振周波
数を基準発振器から供給される共通の原振周波数を用い
て生成することにより同様の作用を得ることができる。
In the case of a configuration in which the uplink frequency is converted into the downlink frequency by using a plurality of frequency converters, the local oscillation frequency used for each frequency converter is a common source supplied from the reference oscillator. A similar effect can be obtained by generating using the vibration frequency.

【0013】[0013]

【実施例】以下、本発明の実施例を図によって説明す
る。図2は、本発明の一実施例を示したものであり、シ
ングルビーム、シングルコンバージョン方式の衛星搭載
中継器の構成の例であって、2-1は局部発振系、3 -1
ミキサ、4-1はRF系入力部、5-1はRF系出力部、6
-1は周波数変換器、7はビーコン周波数生成系、8はビ
ーコン発振器、9は周波数可変の基準発振器、10は低
雑音増幅器(LNA)、11は電力増幅器(HPA)、
12はビーコン送信機を表わしている。
Embodiments of the present invention will be described below with reference to the drawings.
It FIG. 2 shows an embodiment of the present invention.
Single beam, single beam satellite
It is an example of a structure of a repeater, and is 2-1Is the local oscillation system, 3 -1Is
Mixer, 4-1Is the RF input section, 5-1Is the RF output section, 6
-1Is a frequency converter, 7 is a beacon frequency generation system, and 8 is a
Control oscillator, 9 is a variable frequency reference oscillator, and 10 is low
Noise amplifier (LNA), 11 is a power amplifier (HPA),
Reference numeral 12 represents a beacon transmitter.

【0014】そして、周波数変換器6-1によりアップリ
ンク周波数をダウンリンク周波数に変換する構成を採っ
ている。微弱なアップリンク信号を低雑音で受信、増幅
するための低雑音増幅器(LNA)および、ダウンリン
ク信号の所要の出力を得るための電力増幅器(HPA)
が周波数変換器6-1の前後に接続され、ビーコンの所要
出力を得るためのビーコン送信機8がビーコン発振器7
の後段に接続されて衛星搭載中継器が構成されている。
The frequency converter 6 -1 is used to convert the uplink frequency into the downlink frequency. Low noise amplifier (LNA) for receiving and amplifying weak uplink signal with low noise, and power amplifier (HPA) for obtaining required output of downlink signal
Are connected before and after the frequency converter 6 -1 , and the beacon transmitter 8 for obtaining the required output of the beacon is the beacon oscillator 7
The satellite-mounted repeater is connected to the latter stage.

【0015】図3は本発明の他の実施例を示したもので
あり、シングルビーム、ダブルコンバージョン方式の衛
星搭載中継器の構成の例である。本実施例は、周波数変
換器6-1および周波数変換器6-2により、アップリンク
周波数をダウンリンク周波数に変換する構成の場合を示
している。
FIG. 3 shows another embodiment of the present invention, which is an example of the configuration of a single-beam, double-conversion satellite-mounted repeater. The present embodiment shows a case where the frequency converter 6 -1 and the frequency converter 6 -2 convert the uplink frequency to the downlink frequency.

【0016】図中の数字符号は図2の場合と同様であ
る。
The reference numerals in the figure are the same as those in FIG.

【0017】図2および図3に示した実施例は、いずれ
の構成においても、前記「作用の項」で説明したように
衛星搭載中継器の周波数安定度は、周波数可変の基準発
振器9の周波数安定度にだけ依存し、無変調波であるビ
ーコンの周波数を測定することで通信を継続したまま衛
星搭載中継器の周波数変動の様子をモニタできる。そし
て、ビーコン周波数の偏差を検出し、その偏差が無くな
るように基準発振器の発振周波数を調整することで衛星
搭載中継器の周波数の高安定化が実現できる。
In any of the configurations shown in FIG. 2 and FIG. 3, the frequency stability of the satellite-mounted repeater is the frequency of the frequency-variable reference oscillator 9 as described in the above "Operation" section. By measuring the frequency of the beacon, which is an unmodulated wave, which depends only on the stability, it is possible to monitor the frequency fluctuations of the satellite-mounted repeater while continuing communication. Then, the deviation of the beacon frequency is detected, and the oscillation frequency of the reference oscillator is adjusted so as to eliminate the deviation, whereby the frequency of the repeater mounted on the satellite can be highly stabilized.

【0018】なお、マルチビーム方式衛星搭載中継器、
周波数帯の異なる複数のミッションを搭載する衛星搭載
中継器等どのような構成の衛星搭載中継器においても、
全ての周波数変換器と全てのビーコン発振器の原振周波
数を共通の基準発振器から供給する構成とすることによ
って同様の作用効果を得ることができる。
A multi-beam type satellite-mounted repeater,
In a satellite-mounted repeater of any configuration, such as a satellite-mounted repeater equipped with multiple missions with different frequency bands,
Similar effects can be obtained by adopting a configuration in which the original oscillation frequencies of all frequency converters and all beacon oscillators are supplied from a common reference oscillator.

【0019】[0019]

【発明の効果】以上説明したように、本発明の衛星搭載
中継器は周波数変換器の局部発振器とビーコン発振器を
共通の基準発振器に同期させ、かつ、その基準発振器に
周波数の調整機能を付加しているので周波数安定度が高
い衛星搭載中継器を容易に実現することができ、また、
通信を継続したまま周波数の高安定化を実現できるとい
う利点がある。
As described above, the satellite-mounted repeater of the present invention synchronizes the local oscillator and the beacon oscillator of the frequency converter with a common reference oscillator, and adds a frequency adjusting function to the reference oscillator. Therefore, it is possible to easily realize a satellite-mounted repeater with high frequency stability.
There is an advantage that high frequency stabilization can be realized while continuing communication.

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

【図1】本発明の原理的構成を示す図である。FIG. 1 is a diagram showing a principle configuration of the present invention.

【図2】本発明の一実施例を示す図である。FIG. 2 is a diagram showing an embodiment of the present invention.

【図3】本発明の他の実施例を示す図である。FIG. 3 is a diagram showing another embodiment of the present invention.

【図4】従来の衛星中継器の主要部の構成の例を示す図
である。
FIG. 4 is a diagram showing an example of a configuration of a main part of a conventional satellite repeater.

【符号の説明】[Explanation of symbols]

1,1-1〜1-n+1 基準発振器 2-1〜2-n 周波数変換器の局部発振系 3-1〜3-n 周波数変換器のミキサ 4-1〜4-n 周波数変換器のRF系入力部 5-1〜5-n 周波数変換器のRF系出力部 6-1〜6-n 周波数変換器 7 ビーコン周波数生成系 8 ビーコン発振器 9 周波数可変の基準発振器 10 低雑音増幅器(LNA) 11 電力増幅器(HPA) 12 ビーコン送信機 13 基準発振器の周波数制御手段1, 1 -1 to 1 -n + 1 Reference oscillator 2 -1 to 2 -n Local oscillator system of frequency converter 3 -1 to 3 -n Mixer of frequency converter 4 -1 to 4 -n Frequency converter RF system input section 5 -1 to 5 -n RF converter output section of frequency converter 6 -1 to 6 -n frequency converter 7 Beacon frequency generation system 8 Beacon oscillator 9 Frequency variable reference oscillator 10 Low noise amplifier (LNA) 11 Power Amplifier (HPA) 12 Beacon Transmitter 13 Reference Oscillator Frequency Control Means

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 アップリンク周波数をダウンリンク周波
数に変換する周波数変換手段と、ビーコン発振手段を有
する衛星搭載中継器において、 前記周波数変換手段の局部発振器の発振周波数、およ
び、前記ビーコン発振手段の発振周波数を、一つの基準
発振器の発振周波数を基準に決定すると共に、 前記一つの基準発振器の発振周波数を、任意に変化させ
る手段を備えたことを特徴とする衛星搭載中継器。
1. A satellite transponder having frequency conversion means for converting an uplink frequency into a downlink frequency and beacon oscillating means, wherein an oscillation frequency of a local oscillator of the frequency converting means and an oscillation of the beacon oscillating means. A satellite-borne repeater, comprising means for determining a frequency on the basis of an oscillation frequency of one reference oscillator and arbitrarily changing the oscillation frequency of the one reference oscillator.
JP13855392A 1992-05-29 1992-05-29 Satellite-mounted repeater Pending JPH05336012A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13855392A JPH05336012A (en) 1992-05-29 1992-05-29 Satellite-mounted repeater

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13855392A JPH05336012A (en) 1992-05-29 1992-05-29 Satellite-mounted repeater

Publications (1)

Publication Number Publication Date
JPH05336012A true JPH05336012A (en) 1993-12-17

Family

ID=15224837

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13855392A Pending JPH05336012A (en) 1992-05-29 1992-05-29 Satellite-mounted repeater

Country Status (1)

Country Link
JP (1) JPH05336012A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007028374A (en) * 2005-07-20 2007-02-01 Nippon Antenna Co Ltd TV broadcast retransmitter
JP2011508552A (en) * 2007-12-28 2011-03-10 アストリウム・リミテッド Communication channel filtering for telecommunications satellites

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5296813A (en) * 1976-02-09 1977-08-15 Nippon Telegr & Teleph Corp <Ntt> Transbonder for loading satelite
JPS61220534A (en) * 1985-03-27 1986-09-30 Nec Corp One-frequency repeater

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5296813A (en) * 1976-02-09 1977-08-15 Nippon Telegr & Teleph Corp <Ntt> Transbonder for loading satelite
JPS61220534A (en) * 1985-03-27 1986-09-30 Nec Corp One-frequency repeater

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007028374A (en) * 2005-07-20 2007-02-01 Nippon Antenna Co Ltd TV broadcast retransmitter
JP4606958B2 (en) * 2005-07-20 2011-01-05 日本アンテナ株式会社 TV broadcast retransmitter
JP2011508552A (en) * 2007-12-28 2011-03-10 アストリウム・リミテッド Communication channel filtering for telecommunications satellites

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