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JPH0728255B2 - Earth station communication equipment - Google Patents
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JPH0728255B2 - Earth station communication equipment - Google Patents

Earth station communication equipment

Info

Publication number
JPH0728255B2
JPH0728255B2 JP19368389A JP19368389A JPH0728255B2 JP H0728255 B2 JPH0728255 B2 JP H0728255B2 JP 19368389 A JP19368389 A JP 19368389A JP 19368389 A JP19368389 A JP 19368389A JP H0728255 B2 JPH0728255 B2 JP H0728255B2
Authority
JP
Japan
Prior art keywords
frequency
signal
earth station
transmission
output
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.)
Expired - Lifetime
Application number
JP19368389A
Other languages
Japanese (ja)
Other versions
JPH0357325A (en
Inventor
弘晃 安達
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
Original Assignee
NEC 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 filed Critical NEC Corp
Priority to JP19368389A priority Critical patent/JPH0728255B2/en
Publication of JPH0357325A publication Critical patent/JPH0357325A/en
Publication of JPH0728255B2 publication Critical patent/JPH0728255B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、衛星通信の地球局通信装置に利用する。特
に、複数のチャネルを周波数多重して通信衛星を介して
複数の地球局と通信を行うSCPC方式(Single Channel P
er Carrier方式)の地球局通信装置に関するものであ
る。
DETAILED DESCRIPTION OF THE INVENTION [Industrial field of application] The present invention is used for an earth station communication device for satellite communication. In particular, the SCPC method (Single Channel P) that performs frequency multiplexing of multiple channels and communicates with multiple earth stations via communication satellites.
er Carrier method) earth station communication device.

〔概要〕〔Overview〕

本発明は地球局通信装置において、 所定の周期で短時間の無変調キャリヤを送信し、通信衛
星で折返された無変調キャリヤと送信した無変調キャリ
ヤとの周波数を比較し、この比較結果に基づき受信側周
波数を補正することにより、 規模が小さく安価でチャネル効率が良く、かつ良好なチ
ャネル分離ができるようにしたものである。
The present invention, in an earth station communication device, transmits an unmodulated carrier for a short period of time at a predetermined cycle, compares the frequencies of the unmodulated carrier returned by a communication satellite and the transmitted unmodulated carrier, and based on this comparison result. By correcting the frequency on the receiving side, the scale is small, the cost is low, the channel efficiency is good, and good channel separation is possible.

〔従来の技術〕[Conventional technology]

従来、地球局通信装置は、周波数変換器やフィルタを用
いてチャネルの分離を行っていた。このために、チャネ
ルの帯域に比べて無線周波数が極めて大きな場合には、
周波数変換器等は極めて高い周波数精度が要求される。
この要求を満たすために、従来種々のAFC方式(Automat
ic Frequency Compensation方式)が用いられてきた。
Conventionally, the earth station communication device has performed channel separation using a frequency converter and a filter. For this reason, when the radio frequency is extremely large compared to the band of the channel,
A frequency converter or the like requires extremely high frequency accuracy.
In order to meet this requirement, various conventional AFC methods (Automatic
ic Frequency Compensation method) has been used.

一例としてパイロットキャリヤを用いる方法がある。こ
れは多数チャネルのうち特定チャネルに無変調キャリヤ
を送出し、送出局以外の局はその無変調キャリヤを周波
数基準とする方式である。特に、衛星通信では、衛星ト
ランスポンダの周波数変動や衛星自体のドップラ効果に
よる周波数変動が大きく、回線全体の周波数安定度を所
要の値に抑えるためには、パイロットキャリヤ方式が必
要不可欠なものとなっていた。
As an example, there is a method using a pilot carrier. This is a system in which an unmodulated carrier is transmitted to a specific channel among a large number of channels, and stations other than the transmitting station use the unmodulated carrier as a frequency reference. Especially in satellite communications, frequency fluctuations due to the frequency fluctuations of the satellite transponder and the Doppler effect of the satellite itself are large, and the pilot carrier method is indispensable to suppress the frequency stability of the entire line to the required value. It was

〔発明が解決しようとする問題点〕[Problems to be solved by the invention]

しかし、このような従来の地球局通信装置では、パイロ
ットキャリヤを用いるAFC方式であるために、パイロッ
トキャリヤ専用の送信装置および受信装置が必要で装置
規模が大きく、小容量の通信局ではその占める比率は無
視できずまた高価な欠点があった。
However, in such a conventional earth station communication device, since it is an AFC system using a pilot carrier, a transmission device and a reception device dedicated to the pilot carrier are required, and the device scale is large. Has a drawback that is not negligible and expensive.

また、パイロットキャリヤのために周波数帯域を通常1
チャネル分占有することになり、本来の通信に用いるチ
ャネル数が減少する欠点があった。
Also, the frequency band is usually set to 1 for the pilot carrier.
There is a drawback that the number of channels used for the original communication is reduced because the channels are occupied.

本発明は上記の欠点を解決するもので、規模が小さく安
価でチャネル効率が良く、かつ良好なチャネル分離がで
きる地球局通信装置を提供することを目的とする。
The present invention solves the above-mentioned drawbacks, and an object of the present invention is to provide an earth station communication device that is small in scale, inexpensive, has good channel efficiency, and can perform good channel separation.

〔問題点を解決するための手段〕[Means for solving problems]

本発明は、入力する送信ベースバンド信号に基づいて複
数のチャネルのそれぞれの周波数を変調する変調手段
と、この変調手段の出力信号を通信衛星に送信する送信
手段と、この通信衛星の出力信号を受信する受信手段
と、この受信手段の出力信号を上記各チャネルごとに復
調して受信ベースバンド信号を出力する復調手段と、上
記変調手段およびこの復調手段の周波数分割制御を行う
周波数制御手段とを備えた地球局通信装置において、上
記周波数制御手段は、所定の周期で短時間上記送信ベー
スバンド信号を上記変調手段に与えることを中断してそ
の期間に無変調キャリヤを送出させる手段と、この送出
された無変調キャリヤが上記通信衛星により折返された
信号を上記復調手段から入力しその信号の周波数変動を
検出する手段と、この検出する手段の検出結果に基づい
て上記受信手段の出力周波数の制御を行う手段とを含む
ことを特徴とする。
The present invention provides a modulation means for modulating each frequency of a plurality of channels based on an input transmission baseband signal, a transmission means for transmitting an output signal of the modulation means to a communication satellite, and an output signal of the communication satellite. Receiving means for receiving, demodulating means for demodulating the output signal of the receiving means for each of the channels to output a received baseband signal, the modulating means and frequency control means for performing frequency division control of the demodulating means. In the earth station communication device provided, the frequency control means interrupts the application of the transmission baseband signal to the modulation means for a short period of time at a predetermined cycle and sends out an unmodulated carrier during the period, and the sending means. Means for inputting from the demodulation means a signal in which the unmodulated carrier is returned by the communication satellite, and detecting a frequency fluctuation of the signal; Based on the detection result of the means for output, characterized in that it comprises a means for controlling the output frequency of said receiving means.

〔作用〕[Action]

周波数制御手段は所定の周期で短時間送信ベースバンド
信号を変調手段に与えることを中断してその期間に無変
調キャリヤを送出させる。またこの送出された無変調キ
ャリヤが通信衛星を介して折返された信号を復調手段か
ら入力しその信号と送出したときの無変調キャリヤとの
周波数を比較して周波数変動を検出する。さらにこの検
出結果に基づいて次の無変調キャリヤを送出するまでの
期間受信手段の出力周波数を制御する。以上の動作によ
り規模が小さく安価でチャネル効率が良く、かつ良好な
チャネル分離ができる。
The frequency control means interrupts the application of the short-time transmission baseband signal to the modulation means at a predetermined cycle, and causes the non-modulated carrier to be transmitted during that period. Further, a signal returned from the unmodulated carrier sent out via the communication satellite is input from the demodulation means, and the frequency of the signal is compared with the frequency of the unmodulated carrier when sent out to detect the frequency fluctuation. Further, based on this detection result, the output frequency of the receiving means is controlled during the period until the next non-modulated carrier is transmitted. By the above operation, the scale is small, the cost is low, the channel efficiency is good, and the good channel separation can be performed.

〔実施例〕〔Example〕

本発明の実施例について図面を参照して説明する。第1
図は本発明一実施例地球局通信装置のブロック構成図で
ある。第1図において、地球局通信装置は、入力する送
信ベースバンド信号に基づいて複数のチャネルのそれぞ
れの周波数を変調する変調手段として送信側シンセサイ
ザ回路6および変調器7と、この変調器7の出力信号を
通信衛星に送信する送信手段として送信周波数変換器
3、フィーダ回路2の一部およびアンテナ1の一部と、
この通信衛星の出力信号を受信する受信手段としてアン
テナ1の一部、フィーダ回路2の一部および受信周波数
変換器4と、受信周波数変換器4の出力信号を上記各チ
ャネルごとに復調して受信ベースバンド信号を出力する
復調手段として受信側シンセサイザ回路9および復調器
8と、変調器7および復調器8の周波数分割制御を行う
周波数制御手段として周波数制御回路11の一部とを備え
る。
Embodiments of the present invention will be described with reference to the drawings. First
FIG. 1 is a block diagram of an earth station communication device according to an embodiment of the present invention. In FIG. 1, the earth station communication device includes a transmitter-side synthesizer circuit 6 and a modulator 7 as a modulator that modulates respective frequencies of a plurality of channels based on an input transmission baseband signal, and an output of the modulator 7. A transmission frequency converter 3, a part of the feeder circuit 2 and a part of the antenna 1 as transmission means for transmitting a signal to a communication satellite;
As a receiving means for receiving the output signal of the communication satellite, a part of the antenna 1, a part of the feeder circuit 2, the reception frequency converter 4, and the output signal of the reception frequency converter 4 are demodulated and received for each channel. The receiving side synthesizer circuit 9 and the demodulator 8 are provided as demodulation means for outputting a baseband signal, and a part of the frequency control circuit 11 is provided as frequency control means for performing frequency division control of the modulator 7 and the demodulator 8.

ここで本発明の特徴とするところは、周波数制御手段
は、所定の周期で短時間上記送信ベースバンド信号を変
調器7に与えることを中断してその期間に無変調キャリ
ヤを送出させる手段として切替器10および周波数制御回
路11の一部と、この送出された無変調キャリヤが上記通
信衛星により折返された信号を復調器8から入力しその
信号の周波数変動を検出する手段として周波数制御回路
11の一部と、この検出する手段の検出結果に基づいて受
信周波数変換器4の出力周波数の制御を行う手段として
電圧制御発振器5および周波数制御回路11の一部とを含
むことにある。
Here, the feature of the present invention is that the frequency control means is switched as a means for interrupting the application of the transmission baseband signal to the modulator 7 for a short period of time at a predetermined cycle and transmitting an unmodulated carrier during that period. A part of the frequency control circuit 11 and the frequency control circuit 11 and a frequency control circuit as means for inputting from the demodulator 8 a signal in which the transmitted unmodulated carrier is returned by the communication satellite and detecting the frequency fluctuation of the signal.
11 and a part of the voltage control oscillator 5 and the frequency control circuit 11 as a means for controlling the output frequency of the reception frequency converter 4 based on the detection result of the detecting means.

このような構成の地球局通信装置の動作について説明す
る。第2図は本発明の地球局通信装置の無変調キャリヤ
の送受信タイミングを示す図である。第1図において、
通信データの送信時には、送信ベースバンド装置より入
力された送信信号は、切替器10を通った後に変調器7に
より変調される。次に送信側シンセサイザ回路6により
無線チャネルを選択された後に送信周波数変換器3、フ
ィーダ回路2およびアンテナ1を介して通信衛星に送信
される。
The operation of the earth station communication device having such a configuration will be described. FIG. 2 is a diagram showing the transmission / reception timing of the unmodulated carrier of the earth station communication apparatus of the present invention. In FIG.
When transmitting communication data, a transmission signal input from the transmission baseband device is modulated by the modulator 7 after passing through the switch 10. Next, a radio channel is selected by the transmitting side synthesizer circuit 6 and then transmitted to the communication satellite via the transmitting frequency converter 3, the feeder circuit 2 and the antenna 1.

一方、通信データの受信時はアンテナ1とフィーダ回路
2を通った後に受信周波数変換器4を通った後に復調器
8で復調される。ここで、受信チャネルは受信側シンセ
サイザ回路9により選択される。復調器8の出力は受信
ベースバンド装置へ出力される。
On the other hand, when receiving communication data, it is demodulated by the demodulator 8 after passing through the antenna 1 and the feeder circuit 2 and then through the receiving frequency converter 4. Here, the receiving channel is selected by the receiving side synthesizer circuit 9. The output of the demodulator 8 is output to the receiving baseband device.

なお本実施例では簡単のため変復調部が1回路のみ示さ
れているが多数の変復調部を周波数変換器に接続し周波
数多重も可能である。
Although only one modulation / demodulation unit is shown in this embodiment for simplicity, frequency modulation can be performed by connecting a large number of modulation / demodulation units to a frequency converter.

一方、本実施例で与えられる周波数制御回路11は、送信
側シンセサイザ回路6および受信側シンセサイザ回路9
の周波数制御を行う手段をもつ。また、切替器10を制御
することにより無変調キャリヤを送信する手段をもつ。
さらに受信周波数変換器4の出力信号を入力し、周波数
をカウントするカウント手段をもつ。また上記カウント
手段で得られた周波数と本来の周波数との差分を検出
し、それを補償するために電圧制御発振器5を制御する
手段をもつ。
On the other hand, the frequency control circuit 11 provided in this embodiment includes a transmitter side synthesizer circuit 6 and a receiver side synthesizer circuit 9.
It has a means to control the frequency. It also has means for transmitting the unmodulated carrier by controlling the switch 10.
Further, it has a counting means for inputting the output signal of the reception frequency converter 4 and counting the frequency. It also has means for detecting the difference between the frequency obtained by the counting means and the original frequency and controlling the voltage controlled oscillator 5 to compensate for it.

次に本発明による自局内折返しによる自動周波数補償の
方法について説明する。周波数制御回路11は所定の周期
毎に切替器10を制御し、強制的に無変調キャリヤを作
る。この無変調キャリヤ送出時間は、短時間でよく、ま
た周波数制御回路11のカウント手段がカウントできる程
度の時間で良い。また、無変調キャリヤの送出周期は、
周波数変動の支配的要素が通信衛星および送受信周波数
変換器でありそれらが短期的変動よりは長期的変動であ
る点を考慮し、たとえば1時間周期程度の長時間に選択
される。
Next, a method of automatic frequency compensation by folding back in the own station according to the present invention will be described. The frequency control circuit 11 controls the switch 10 at every predetermined cycle to forcibly make an unmodulated carrier. This non-modulated carrier sending time may be a short time, and may be a time such that the counting means of the frequency control circuit 11 can count. Also, the transmission cycle of the unmodulated carrier is
Considering that the communication satellite and the transmission / reception frequency converter are the dominant elements of the frequency fluctuation and they are long-term fluctuations rather than short-term fluctuations, they are selected for a long time, for example, about one hour period.

次に、自局折返しによる周波数補正は第2図に示すタニ
ミングにて行われる。第2図(a)において、TNは無変
調キャリヤ送出時間を示す。無変調キャリヤを受信する
ため受信側シンセサイザ回路9を送信側と同一チャネル
に切換えるがそのタイミングを示したものが第2図
(b)である。すなわち、通信衛星による遅延時間TD
だけ遅らせた後に無変調キャリヤ送出時間TNの時間のみ
送受同一チャネルとなっている。無変調キャリヤの受信
時には、瞬時に周波数制御回路11のカウント手段のゲー
トが開き、周波数をカウントし、その結果本来の周波数
との比較によりその周波数差分に相当する電圧を電圧制
御発振器5に与える。
Next, the frequency correction by the loopback of the own station is performed by the tanning shown in FIG. In FIG. 2 (a), T N represents the non-modulated carrier transmission time. In order to receive the unmodulated carrier, the receiving side synthesizer circuit 9 is switched to the same channel as the transmitting side, and the timing is shown in FIG. 2 (b). That is, the transmission and reception are on the same channel only after the delay time T D due to the communication satellite and the unmodulated carrier transmission time T N. Upon reception of an unmodulated carrier, the gate of the counting means of the frequency control circuit 11 instantly opens and counts the frequency. As a result, the voltage corresponding to the frequency difference is applied to the voltage controlled oscillator 5 by comparison with the original frequency.

以上で自局内周波数補正が完了し、完了と同時に通常の
データ送受信状態となる。この場合に電圧制御発振器5
の制御電圧は、周波数制御回路11によって記憶され次の
周波数補正時まで同一制御電圧を使用する。
With the above, the frequency correction in the own station is completed, and upon completion, the normal data transmission / reception state is set. In this case, the voltage controlled oscillator 5
The control voltage is stored by the frequency control circuit 11 and the same control voltage is used until the next frequency correction.

上述した自局内周波数補正を各地球局が行うことにより
衛星トランスポンダの周波数変動や受信系高周波回路の
周波数変動を抑えることができる。
By performing the above-described in-station frequency correction by each earth station, it is possible to suppress the frequency fluctuation of the satellite transponder and the frequency fluctuation of the receiving system high frequency circuit.

なお本実施例は自局折返しによる周波数補正を行ってい
るために各地球局間の通信では各送信系が自局折返し時
と異なるため周波数補正されないことになる。このため
に各地球局の送信側高周波回路すなわち送信周波数変換
器3の周波数偏差を少なくして各地球局間の周波数誤差
をなくすことが必要である。
Since the frequency correction is performed by the return of the own station in this embodiment, the frequency is not corrected in the communication between the respective earth stations because each transmission system is different from that at the time of the return of the own station. Therefore, it is necessary to reduce the frequency deviation of the transmitting side high frequency circuit of each earth station, that is, the transmission frequency converter 3 to eliminate the frequency error between the earth stations.

〔発明の効果〕〔The invention's effect〕

以上説明したように、本発明は、高価なパイロットキャ
リヤ方式を使用せず規模が小さく安価な制御回路で正確
な受信ができる優れた高価がある。また電圧制御発振器
を高い周波数精度で制御することが不必要な利点があ
る。
As described above, the present invention is excellent in cost because accurate control can be performed with a small-scale and inexpensive control circuit without using an expensive pilot carrier system. Further, there is an advantage that it is unnecessary to control the voltage controlled oscillator with high frequency accuracy.

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

第1図は本発明一実施例地球局通信装置のブロック構成
図。 第2図は本発明の地球局通信装置の無変調キャリヤの送
受信タイミングを示す図。 1……アンテナ、2……フィーダ回路、3……送信周波
数変換器、4……受信周波数変換器、5……電圧制御発
振器、6……送信側シンセサイザ回路、7……変調器、
8……復調器、9……受信側シンセサイザ回路、10……
切替器、11……周波数制御回路。
FIG. 1 is a block diagram of an earth station communication device according to an embodiment of the present invention. FIG. 2 is a diagram showing a transmission / reception timing of an unmodulated carrier of the earth station communication device of the present invention. 1 ... Antenna, 2 ... Feeder circuit, 3 ... Transmission frequency converter, 4 ... Reception frequency converter, 5 ... Voltage controlled oscillator, 6 ... Transmitting side synthesizer circuit, 7 ... Modulator,
8 ... Demodulator, 9 ... Receiving side synthesizer circuit, 10 ...
Switching device, 11 ... Frequency control circuit.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】入力する送信ベースバンド信号に基づいて
複数のチャネルのそれぞれの周波数を変調する変調手段
と、この変調手段の出力信号を通信衛星に送信する送信
手段と、この通信衛星の出力信号を受信する受信手段
と、この受信手段の出力信号を上記各チャネルごとに復
調して受信ベースバンド信号を出力する復調手段と、上
記変調手段およびこの復調手段の周波数分割制御を行う
周波数制御手段とを備えた 地球局通信装置において、 上記周波数制御手段は、所定の周期で短時間上記送信ベ
ースバンド信号を上記変調手段に与えることを中断して
その期間に無変調キャリヤを送出させる手段と、この送
出された無変調キャリヤが上記通信衛星により折返され
た信号を上記復調手段から入力しその信号の周波数変動
を検出する手段と、この検出する手段の検出結果に基づ
いて上記受信手段の出力周波数の制御を行う手段とを含
む ことを特徴とする地球局通信装置。
1. A modulation means for modulating each frequency of a plurality of channels based on an input transmission baseband signal, a transmission means for transmitting an output signal of the modulation means to a communication satellite, and an output signal of the communication satellite. Receiving means, a demodulating means for demodulating an output signal of the receiving means for each channel to output a received baseband signal, a modulating means and a frequency control means for performing frequency division control of the demodulating means. In the earth station communication device provided with, the frequency control means, means for interrupting the application of the transmission baseband signal to the modulation means for a short period of time at a predetermined period, and sending an unmodulated carrier during the period, Means for inputting from the demodulation means a signal in which the transmitted unmodulated carrier is returned by the communication satellite, and detecting a frequency fluctuation of the signal; Detection for earth station communication apparatus characterized by comprising means for controlling the output frequency of said receiving means based on a detection result of means.
JP19368389A 1989-07-25 1989-07-25 Earth station communication equipment Expired - Lifetime JPH0728255B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19368389A JPH0728255B2 (en) 1989-07-25 1989-07-25 Earth station communication equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19368389A JPH0728255B2 (en) 1989-07-25 1989-07-25 Earth station communication equipment

Publications (2)

Publication Number Publication Date
JPH0357325A JPH0357325A (en) 1991-03-12
JPH0728255B2 true JPH0728255B2 (en) 1995-03-29

Family

ID=16312052

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19368389A Expired - Lifetime JPH0728255B2 (en) 1989-07-25 1989-07-25 Earth station communication equipment

Country Status (1)

Country Link
JP (1) JPH0728255B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5226491B2 (en) * 2008-12-09 2013-07-03 パナソニック株式会社 Wireless communication system

Also Published As

Publication number Publication date
JPH0357325A (en) 1991-03-12

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