JPH0229034A - Receiver - Google Patents

Receiver

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Publication number
JPH0229034A
JPH0229034A JP17941988A JP17941988A JPH0229034A JP H0229034 A JPH0229034 A JP H0229034A JP 17941988 A JP17941988 A JP 17941988A JP 17941988 A JP17941988 A JP 17941988A JP H0229034 A JPH0229034 A JP H0229034A
Authority
JP
Japan
Prior art keywords
signal
level
frequency
output
pilot
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
JP17941988A
Other languages
Japanese (ja)
Inventor
Hiromi Shimoda
下田 弘美
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 JP17941988A priority Critical patent/JPH0229034A/en
Publication of JPH0229034A publication Critical patent/JPH0229034A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To prevent a level of other reception signal from being exceeded due to the level reduction of a pilot signal by using a branch circuit so as to branch part of the reception signal outputted to a demodulator of the post- stage, applying level control to the branched output by a level control means and inputting the result. CONSTITUTION:A pilot level detector 5 is a narrow band detector in a receiver installed in the satellite communication earth station employing the SCPC system, only a pilot signal in an output signal of a variable attenuator 3 is detected and the detection output is digitized by an A/D converter 6 and inputted to a control circuit 7. The control circuit 7 compares the digital value with a reference value and since the attenuation of the variable attenuator 3 is controlled by an analog signal in a direction where the error is decrease, the level of the pilot signal given to a pilot frequency detector 4 is nearly kept constant. The control circuit 7 detects whether or not the error is within a prescribed range and if the error is deviated from the prescribed range, it is discriminated that the pilot signal reception is interrupted.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は受信装置に関し、特にFDMA方式をとる衛星
通信地球局の受信装置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a receiving device, and particularly to a receiving device for a satellite communication earth station that uses the FDMA system.

〔従来の技術〕[Conventional technology]

FDMA方式をとる衛星通信地球局の受信装置、中でも
SCPC(single channel  per 
carrier)方式におけるように比較的狭帯域の信
号を受信する受信装置は、受信信号中に含まれるパイロ
ット信号が一定の周波数の中間周波信号に周波数変換さ
れるように周波数変換器の局部発振器の発振周波数を制
御するのが通例である。パイロット信号は基準地球局か
ら高い周波数確度で送出され、宇宙局で中継される。各
送信地球局から送出され宇宙局で中継された各受信信号
は、上記の周波数変換器で共通に周波数変換され、それ
ぞれ所定の周波数の中間周波数信号になり、後段の各チ
ャネルの復調装置へ出力される。この周波数変換により
、宇宙局での中継の際に発生した各受信信号の周波数誤
差も共通に補正される。
Receiving equipment for satellite communication earth stations that use the FDMA method, especially SCPC (single channel per
A receiving device that receives a relatively narrow band signal such as in the carrier system uses the oscillation of a local oscillator of a frequency converter so that the pilot signal included in the received signal is frequency-converted into an intermediate frequency signal with a constant frequency. It is customary to control the frequency. The pilot signal is transmitted from the reference earth station with high frequency accuracy and relayed by the space station. Each received signal sent from each transmitting earth station and relayed by the space station is commonly frequency-converted by the above frequency converter, becomes an intermediate frequency signal of a predetermined frequency, and is output to the demodulator of each channel in the subsequent stage. be done. Through this frequency conversion, frequency errors in each received signal that occur during relay at the space station are also commonly corrected.

中間周波帯のパイロット信号の周波数を周波数検出器で
検出し、検出結果に基づき局部発振周波数を制御してパ
イロット信号の周波数を一定にするためには、周波数検
出器が正確に周波数検出できるようにそのパイロット入
力レベルを一定に保つ必要がある。
In order to detect the frequency of the pilot signal in the intermediate frequency band with a frequency detector and control the local oscillation frequency based on the detection result to keep the frequency of the pilot signal constant, the frequency detector must be able to accurately detect the frequency. It is necessary to keep the pilot input level constant.

従来のかかる受信装置は、周波数変換器で共通に周波数
変換した各受信信号を共通の可変減衰器でレベル制御し
、レベル制御した各受信信号中のパイロット信号が一定
のレベルになるように可変減衰器を制御することにより
、周波数検出器に入力するパイロットレベルを一定にし
ていた。
Such a conventional receiving device uses a common variable attenuator to control the level of each received signal whose frequency has been commonly converted by a frequency converter, and performs variable attenuation so that the pilot signal in each level-controlled received signal is at a constant level. By controlling the frequency detector, the pilot level input to the frequency detector was kept constant.

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

上述した従来の受信装置は、各受信信号を共通の可変減
衰器でレベル制御して復調装置へ出方するようになって
いるので、基準地球局周辺の降雨による信号減衰等によ
って各受信信号中のパイロット信号のみ受信レベルが低
下すると、このレベル低下を補償するように可変減衰器
が制御され、他の受信信号の出力レベルが過大となって
後段の復調装置が正常に動作しなくなる欠点がある。又
、パイロット信号の降雨減衰等が大きくなってパイロッ
ト信号の受信所になると局部発振器がフリーランになる
ので、受信所中の周波数ドリフトが大きくなると受信回
復時の周波数引込みに長い時間がかかるという欠点があ
る。
In the conventional receiving device described above, the level of each received signal is controlled by a common variable attenuator before outputting it to the demodulator. If the received level of only the pilot signal decreases, the variable attenuator is controlled to compensate for this level drop, and the output level of the other received signals becomes excessive, causing the subsequent demodulator to malfunction. . Additionally, the local oscillator becomes free-running when the pilot signal is attenuated by rain, etc., and becomes a pilot signal receiving station, so if the frequency drift in the receiving station becomes large, it takes a long time to pull in the frequency when the reception is restored. There is.

本発明の目的は、パイロット信号のレベル低下によって
他の受信信号の出力レベルが過大になることを防止でき
、パイロット信号の受信所中も局部発振器の周波数ドリ
フトを小さく保つことができる受信装置を提供すること
にある。
An object of the present invention is to provide a receiving device that can prevent the output level of other received signals from becoming excessive due to a drop in the level of a pilot signal, and can keep the frequency drift of a local oscillator small even during a pilot signal reception station. It's about doing.

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

本発明の受信装置は、複数の地球局が送出し宇宙局が中
継した複数の受信信号を中間周波帯に共通に周波数変換
する周波数変換器と、この周波数変換器の出力信号を分
岐する分岐回路と、この分岐回路の分岐出力を第1の制
御信号に基づきレベル制御するレベル制御手段と、この
レベル制御手段の出力信号が含むパイロット信号の周波
数及びレベルを検出する検出手段と、この検出手段のレ
ベル検出結果に基づき前記第1の制御信号を出力し前記
第1の制御信号の値があらかじめ定めた範囲内にあると
きは前記検出手段の周波数検出結果に基づき第2の制御
信号を出力し前記第1の制御信号の値が前記あらかじめ
定めた範囲を逸脱したときはその直前の前記第2の制御
信号の値を保持して出力する制御手段と、前記第2の制
御信号に基づく周波数の局部発振信号を発生して前記周
波数変換器へ出力する局部発振器とを備えている。
The receiving device of the present invention includes a frequency converter that commonly converts the frequency of a plurality of received signals transmitted by a plurality of earth stations and relayed by a space station to an intermediate frequency band, and a branch circuit that branches the output signal of the frequency converter. a level control means for controlling the level of the branch output of the branch circuit based on a first control signal; a detection means for detecting the frequency and level of a pilot signal included in the output signal of the level control means; The first control signal is output based on the level detection result, and when the value of the first control signal is within a predetermined range, the second control signal is output based on the frequency detection result of the detection means, and the second control signal is output based on the frequency detection result of the detection means. control means for holding and outputting the immediately preceding value of the second control signal when the value of the first control signal deviates from the predetermined range; and a local oscillator that generates an oscillation signal and outputs it to the frequency converter.

〔実施例〕〔Example〕

次に、本発明について図面を参照して説明する。 Next, the present invention will be explained with reference to the drawings.

第1図は本発明の一実施例を示すブロック図である 第1図に示す実施例は5cpc方式をとる衛星通信地球
局に設置されるものである。基準地球局が送出したパイ
ロット信号及び各送信地球局が送出した各信号は、宇宙
局で中継され、この地球局のアンテナで受信され、低雑
音増幅器を介して第1図に示す実施例に入力し、その出
力は分岐されて後続する各チャネルの復調装置に入力さ
れる。
FIG. 1 is a block diagram showing one embodiment of the present invention. The embodiment shown in FIG. 1 is installed in a satellite communications earth station that uses the 5 CPC system. The pilot signal sent by the reference earth station and each signal sent by each transmitting earth station are relayed by the space station, received by the antenna of this earth station, and input to the embodiment shown in FIG. 1 via a low-noise amplifier. The output is branched and input to a demodulator for each subsequent channel.

第1図に示す実施例は、各受信信号を中間周波帯に共通
に周波数変換する周波数変換器1と、周波数変換器1の
出力信号を復調装置へ出力すると共に一部を分岐する分
岐回路2と、分岐回路2の分岐出力をレベル制御する可
変減衰器3と、可変減衰器3の出力信号が含むパイロッ
ト信号の周波数及びレベルを検出するパイロット周波数
検出器4及びパイロットレベル検出器5と、パイロット
周波数検出器4及びパイロットレベル検出器5の各検出
信号をディジタル値に変換するA/D変換器6と、A/
D変換器6の2つの出力値に基づき2つのディジタル値
を出力する制御回路7と、制御回路7の一方の出力値を
アナログ信号に変換しこのアナログ信号で可変減衰器3
の減衰量を制御するD/A変換器8と、制御回路7の他
方の出力値をアナログ信号に変換するD/A変換器9と
、D/A変換器9が出力したアナログ信号に基づく周波
数の局部発振信号を発生して周波数変換器1へ出力する
局部発振信器10とを備えて構成されている。
The embodiment shown in FIG. 1 includes a frequency converter 1 that commonly converts the frequency of each received signal into an intermediate frequency band, and a branch circuit 2 that outputs the output signal of the frequency converter 1 to a demodulator and branches a part of it. , a variable attenuator 3 that controls the level of the branch output of the branch circuit 2, a pilot frequency detector 4 and a pilot level detector 5 that detect the frequency and level of the pilot signal included in the output signal of the variable attenuator 3, and a pilot An A/D converter 6 that converts each detection signal of the frequency detector 4 and pilot level detector 5 into digital values;
A control circuit 7 that outputs two digital values based on the two output values of the D converter 6, and a control circuit 7 that converts one output value of the control circuit 7 into an analog signal and uses this analog signal to output the variable attenuator 3.
A D/A converter 8 that controls the amount of attenuation of the control circuit 7, a D/A converter 9 that converts the other output value of the control circuit 7 into an analog signal, and a frequency based on the analog signal outputted by the D/A converter 9. and a local oscillator 10 that generates a local oscillation signal and outputs it to the frequency converter 1.

パイロットレベル検出器5は狭帯域の検波器であり、可
変減衰器3の出力信号中のパイロット信号のみを検波1
.て出力する。この検波出力はA7・′D変換器6でデ
ィジタル化されて制御回路7に入力する。制御回路7は
、入力したこのディジタル値を基準値と比較し、誤差値
を出力する。この誤差値がD/A変換器8でアナログ信
号に変換され、このアナログ信号によって誤差値が減少
する方向に可変減衰器3の減衰量が制御されるので、パ
イロット周波数検出器4に入力するパイロット信号のレ
ベルはほぼ一定に保たれる。制御回路7は、又、誤差値
が一定範囲内にあるかどうかを検出しており、誤差値が
この一定範囲を逸脱するとパイロット信号が受信断にな
ったと判定する。
The pilot level detector 5 is a narrow band detector, and detects only the pilot signal in the output signal of the variable attenuator 3.
.. and output it. This detected output is digitized by the A7/'D converter 6 and input to the control circuit 7. The control circuit 7 compares this input digital value with a reference value and outputs an error value. This error value is converted into an analog signal by the D/A converter 8, and this analog signal controls the attenuation amount of the variable attenuator 3 in a direction that reduces the error value, so that the pilot input to the pilot frequency detector 4 The signal level remains approximately constant. The control circuit 7 also detects whether the error value is within a certain range, and determines that the pilot signal has been cut off when the error value deviates from this certain range.

パイロット周波数検出器5は、入力したパイロット信号
と基準周波数信号とを位相比較する位相比較器であり、
パイロット信号の基準周波数信号に対する位相誤差の形
でパイロット信号の周波数を検出する。パイロット周波
数検出器4が出力した位相誤差は、A/D変換器6でデ
ィジタル化されて制御回路7に入力し、制御回路7中の
位相誤差レジスタの内容を更新する。この位相誤差レジ
スタの内容はD/A変換器9でアナログ信号に変換され
、このアナログ信号によって位相誤差が減少するように
局部発振器10の発振周波数が制御されるので、周波数
変換器1が出力する。バ・イロット信号を始めとする、
中間周波帯の名受信信号の周波数はそれぞれ所定の周波
数に保たれる。
The pilot frequency detector 5 is a phase comparator that compares the phases of the input pilot signal and the reference frequency signal,
The frequency of the pilot signal is detected in the form of a phase error of the pilot signal with respect to a reference frequency signal. The phase error output from the pilot frequency detector 4 is digitized by the A/D converter 6 and input to the control circuit 7, and the contents of the phase error register in the control circuit 7 are updated. The contents of this phase error register are converted into an analog signal by the D/A converter 9, and the oscillation frequency of the local oscillator 10 is controlled by this analog signal to reduce the phase error, so that the frequency converter 1 outputs . Including the Bairot signal,
The frequencies of the received signals in the intermediate frequency band are each maintained at a predetermined frequency.

制御回路7は、D/A変換器8へ出力す誤差値の値から
パイロット信号が受信断であると判断すると、位相誤差
レジスタの内容更新を停止する。
When the control circuit 7 determines from the value of the error value output to the D/A converter 8 that the pilot signal is not received, it stops updating the contents of the phase error register.

従って、パイロット信号が受信断である間、位相誤差レ
ジスタは受信断直前の値を保持しており、局部発振器1
00周波周波数変換器D/A変換器9の出力信号)もパ
イロット信号の受信断直前の値に保たれるので、受信断
中における局部発振器10の周波数ドリフトは小さい。
Therefore, while the reception of the pilot signal is interrupted, the phase error register retains the value immediately before the reception is interrupted, and the local oscillator 1
Since the output signal of the 00 frequency frequency converter (D/A converter 9) is also maintained at the value immediately before the reception of the pilot signal is interrupted, the frequency drift of the local oscillator 10 during reception interruption is small.

以上、第1図に示す実施例の動作について説明した。The operation of the embodiment shown in FIG. 1 has been described above.

なお、レベル制御手段として可変利得増幅器を用いるこ
ともできる。又、パイロット信号の周波数を周波数弁別
器で検出する場合にも本発明を適用して上記実施例にお
けると同様な効果を得ることができる。
Note that a variable gain amplifier can also be used as the level control means. Further, the present invention can be applied to the case where the frequency of the pilot signal is detected by a frequency discriminator, and the same effect as in the above embodiment can be obtained.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明は、後段の復調装置へ出力す
る受信信号の一部を分岐回路で分岐し、分岐出力をレベ
ル制御手段でレベル制御して検出手段へ入力することに
より、パイロット信号のレベル低下によって他の受信信
号のレベルが過大になり後段の復調装置が正常に動作し
なくなるのを防止できる効果があり、又、パイロット信
号が受信断の間、受信断直前の第2の制御信号を制御手
段に保持することにより、この間における局部発振器の
周波数ドリフトを小さく保ちパイロット信号の受信回復
時における局部発振器の周波数引込みを速くできる効果
がある。
As explained above, the present invention branches a part of the received signal to be output to the demodulator at the subsequent stage using a branch circuit, controls the level of the branched output using the level control means, and inputs the level to the detection means. This has the effect of preventing the level of other received signals from becoming excessive due to the level drop, which causes the subsequent demodulator to malfunction, and also prevents the pilot signal from being received while the reception is interrupted or by the second control signal just before the reception is interrupted. By holding this in the control means, it is possible to keep the frequency drift of the local oscillator small during this period and to speed up the frequency pull-in of the local oscillator when the reception of the pilot signal is recovered.

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

第1図は本発明の一実施例を示すブロック図である。 1・・・・・・周波数変換器、2・・・・・・分岐回路
、3・・・・・・可変減衰器、4・・・・・・パイロッ
ト周波数検出器、5・・・・・・パイロットレベル検出
器、6・・・・・・A/D変換器、7・・・・・・制御
回路、8,9・・・・・・D/A変換器、10・・・・
・・局部発振器。 代理人 弁理士  内 原   晋
FIG. 1 is a block diagram showing one embodiment of the present invention. 1... Frequency converter, 2... Branch circuit, 3... Variable attenuator, 4... Pilot frequency detector, 5...・Pilot level detector, 6...A/D converter, 7...Control circuit, 8, 9...D/A converter, 10...
...Local oscillator. Agent Patent Attorney Susumu Uchihara

Claims (1)

【特許請求の範囲】[Claims] 複数の地球局が送出し宇宙局が中継した複数の受信信号
を中間周波帯に共通に周波数変換する周波数変換器と、
この周波数変換器の出力信号を分岐する分岐回路と、こ
の分岐回路の分岐出力を第1の制御信号に基づきレベル
制御するレベル制御手段と、このレベル制御手段の出力
信号が含むパイロット信号の周波数及びレベルを検出す
る検出手段と、この検出手段のレベル検出結果に基づき
前記第1の制御信号を出力し前記第1の制御信号の値が
あらかじめ定めた範囲内にあるときは前記検出手段の周
波数検出結果に基づき第2の制御信号を出力し前記第1
の制御信号の値が前記あらかじめ定めた範囲を逸脱した
ときはその直前の前記第2の制御信号の値を保持して出
力する制御手段と、前記第2の制御信号に基づく周波数
の局部発振信号を発生して前記周波数変換器へ出力する
局部発振器とを備えたことを特徴する受信装置。
a frequency converter that commonly converts the frequency of multiple received signals transmitted by multiple earth stations and relayed by the space station to an intermediate frequency band;
A branch circuit that branches the output signal of this frequency converter, level control means that level-controls the branch output of this branch circuit based on a first control signal, and detection means for detecting a level; and outputting the first control signal based on the level detection result of the detection means, and detecting the frequency of the detection means when the value of the first control signal is within a predetermined range. A second control signal is output based on the result and the first control signal is output.
control means for holding and outputting the immediately preceding value of the second control signal when the value of the control signal deviates from the predetermined range; and a local oscillation signal having a frequency based on the second control signal. a local oscillator that generates and outputs the generated signal to the frequency converter.
JP17941988A 1988-07-18 1988-07-18 Receiver Pending JPH0229034A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17941988A JPH0229034A (en) 1988-07-18 1988-07-18 Receiver

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17941988A JPH0229034A (en) 1988-07-18 1988-07-18 Receiver

Publications (1)

Publication Number Publication Date
JPH0229034A true JPH0229034A (en) 1990-01-31

Family

ID=16065539

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17941988A Pending JPH0229034A (en) 1988-07-18 1988-07-18 Receiver

Country Status (1)

Country Link
JP (1) JPH0229034A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5941295A (en) * 1982-09-02 1984-03-07 Mitsubishi Paper Mills Ltd Production of heat-sensitive paper enhanced in printing property
JPH04172828A (en) * 1990-11-07 1992-06-19 Nec Corp Satellite communication earth station

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5941295A (en) * 1982-09-02 1984-03-07 Mitsubishi Paper Mills Ltd Production of heat-sensitive paper enhanced in printing property
JPH0233312B2 (en) * 1982-09-02 1990-07-26 Mitsubishi Paper Mills Ltd
JPH04172828A (en) * 1990-11-07 1992-06-19 Nec Corp Satellite communication earth station

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