JP3042083B2 - Earth station receiver - Google Patents

Earth station receiver

Info

Publication number
JP3042083B2
JP3042083B2 JP3264385A JP26438591A JP3042083B2 JP 3042083 B2 JP3042083 B2 JP 3042083B2 JP 3264385 A JP3264385 A JP 3264385A JP 26438591 A JP26438591 A JP 26438591A JP 3042083 B2 JP3042083 B2 JP 3042083B2
Authority
JP
Japan
Prior art keywords
sweep
signal
voltage
oscillation
unit
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
JP3264385A
Other languages
Japanese (ja)
Other versions
JPH05110484A (en
Inventor
文明 鈴木
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 JP3264385A priority Critical patent/JP3042083B2/en
Publication of JPH05110484A publication Critical patent/JPH05110484A/en
Application granted granted Critical
Publication of JP3042083B2 publication Critical patent/JP3042083B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明は地球局受信装置に関し、
特に通信衛星を介して周波数分割多重信号を受信する地
球局受信装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an earth station receiver.
In particular, the present invention relates to an earth station receiving apparatus for receiving a frequency division multiplexed signal via a communication satellite.

【0002】[0002]

【従来の技術】通信衛星を介して周波数分割多重信号を
受信する場合、通信衛星本体での周波数変動が信号の伝
送速度に比して相対的に大きくなると受信できなくな
る。このため、従来は、システムの基準局側から伝送信
号とは別なシステムパイロット信号を送出し、地球局受
信装置側では、このシステムパイロット信号と基準発振
信号とを比較して局部発振周波数を制御する自動周波数
制御装置(AFC)を追加することにより、通信衛星本
体での周波数変動を相殺して復調している。また、地球
局受信装置の復調器にAFC機能を設け、通信衛星本体
の周波数変動の最大値以上にAFCの引込み範囲を拡張
することも行われている。
2. Description of the Related Art When a frequency division multiplexed signal is received via a communication satellite, the signal cannot be received if the frequency fluctuation in the communication satellite body becomes relatively large compared to the transmission speed of the signal. For this reason, conventionally, a system pilot signal different from the transmission signal is transmitted from the reference station side of the system, and the earth station receiver compares the system pilot signal with the reference oscillation signal to control the local oscillation frequency. By adding an automatic frequency controller (AFC), demodulation is performed by canceling out frequency fluctuations in the communication satellite body. Also, an AFC function is provided in the demodulator of the earth station receiving device, and the AFC pull-in range is extended beyond the maximum value of the frequency fluctuation of the communication satellite body.

【0003】[0003]

【発明が解決しようとする課題】上述したように、通信
衛星本体での周波数変動に対処するためにAFCを設け
ので、装置構成が複雑となり高価になるという問題点が
ある。また、AFCの引込み範囲を拡張する場合、隣接
する伝送信号に誤同期する可能性があるので、伝送信号
の間隔を通信衛星本体の周波数変動の最大値以上に設定
する必要があり、このため、伝送帯域での周波数使用効
率が低下するという問題点を有している。
As described above, since the AFC is provided in order to cope with the frequency fluctuation in the communication satellite main body, there is a problem that the device configuration is complicated and the cost is high. In addition, when extending the AFC pull-in range, there is a possibility of erroneous synchronization with an adjacent transmission signal. Therefore, it is necessary to set the interval between the transmission signals to be equal to or more than the maximum value of the frequency fluctuation of the communication satellite body. There is a problem that the frequency use efficiency in the transmission band is reduced.

【0004】本発明の目的は、専用のAFCを設けるこ
となく、且つ通信衛星本体の周波数変動の最大値以上に
AFCの引込み範囲を拡張することなく、通信衛星本体
の周波数変動に対応できる地球局受信装置を提供するこ
とにある。
SUMMARY OF THE INVENTION It is an object of the present invention to provide an earth station capable of coping with a frequency fluctuation of a communication satellite main body without providing a dedicated AFC and without extending an AFC pull-in range beyond a maximum frequency fluctuation of the communication satellite main body. A receiving device is provided.

【0005】[0005]

【課題を解決するための手段】本発明の地球局受信装置
は、受信信号を中間周波信号に変換する周波数変換部
と、発振制御電圧に応じた周波数の発振信号を出力する
電圧制御発振部と、前記発振信号に応じて前記中間周波
信号を復調して復調信号を出力する復調部と、前記発振
信号と前記中間周波信号との位相差を検出して位相差電
圧を生成する位相比較部と、前記電圧制御発振部の発振
周波数を掃引するために所定の電圧範囲で変化する掃引
電圧を生成する掃引制御部と、前記位相差電圧と前記掃
引電圧とを加算して前記発振制御電圧を生成する加算部
と、前記復調信号の所定の信号と前記発振信号とが同期
したときを検知する同期検知部と、前記掃引電圧の値を
記憶するメモリ部とを備えている。また、前記掃引制御
部は、動作開始時、前記発振信号が前記通信衛星側の周
波数変動の最大値を超えて掃引するように前記掃引電圧
を大きく変化させ、また前記同期検知部が、基準局から
送出されたシステムパイロット信号と前記発振信号との
同期を検知したときに掃引を停止し、掃引停止時の掃引
電圧の値を前記メモリ部に記憶させ、その後、前記メモ
リ部に記憶させた前記掃引停止時の掃引電圧の値を中心
に小さく前記掃引電圧を変化させ、前記同期検知部が、
希望信号と前記発振信号との同期を検知したときに掃引
を停止するように構成する。
According to the present invention, there is provided an earth station receiving apparatus comprising: a frequency converter for converting a received signal into an intermediate frequency signal; and a voltage controlled oscillator for outputting an oscillation signal having a frequency corresponding to an oscillation control voltage. A demodulation unit that demodulates the intermediate frequency signal in accordance with the oscillation signal and outputs a demodulated signal, and a phase comparison unit that detects a phase difference between the oscillation signal and the intermediate frequency signal and generates a phase difference voltage. A sweep control unit that generates a sweep voltage that changes in a predetermined voltage range to sweep the oscillation frequency of the voltage control oscillator, and generates the oscillation control voltage by adding the phase difference voltage and the sweep voltage. An adder that performs synchronization, a synchronization detector that detects when a predetermined signal of the demodulated signal is synchronized with the oscillation signal, and a memory that stores a value of the sweep voltage. Further, at the start of the operation, the sweep control unit greatly changes the sweep voltage so that the oscillation signal sweeps beyond the maximum value of the frequency variation on the communication satellite side, and the synchronization detection unit, from the reference station, When the synchronization between the transmitted system pilot signal and the oscillation signal is detected, the sweep is stopped, the value of the sweep voltage at the time of stopping the sweep is stored in the memory unit, and then the sweep stored in the memory unit is performed. The sweep voltage is changed small around the value of the sweep voltage at the time of stop, the synchronization detection unit,
The sweep is stopped when the synchronization between the desired signal and the oscillation signal is detected.

【0006】[0006]

【実施例】次に本発明について図面を参照して説明す
る。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Next, the present invention will be described with reference to the drawings.

【0007】図1は本発明の一実施例を示すブロック図
である。受信信号S1は、周波数変換部1で局部発振部
2からの局発信号と混合されて所定の中間周波信号S2
に変換され、復調部3により復調されて復調信号S3と
して出力される。ここで、局部発振部2は、例えば周波
数シンセサイザであり、制御部10からの制御信号C1
によって指定された周波数の局発信号を送出する。
FIG. 1 is a block diagram showing one embodiment of the present invention. The reception signal S1 is mixed with a local oscillation signal from the local oscillation unit 2 by the frequency conversion unit 1 to generate a predetermined intermediate frequency signal S2.
And demodulated by the demodulation unit 3 and output as a demodulated signal S3. Here, the local oscillation unit 2 is, for example, a frequency synthesizer, and a control signal C1 from the control unit 10.
Sends out a local oscillation signal of the frequency designated by.

【0008】また、本発明の地球局受信装置は、発振制
御電圧Vcに応じた周波数で発振して発振信号Svを出
力する電圧制御発振部(VCO)4と、発振信号Svと
中間周波信号S2との位相差を検出して位相差電圧Vp
を生成する位相比較部5と、復調信号S3から所定の信
号を検出して発振信号Svと同期したときを検知する同
期検知部6と、電圧制御発振部4の発振周波数を掃引す
る掃引電圧Vsを生成する掃引制御部7と、位相差電圧
Vpと掃引電圧Vsとを加算して発振制御電圧Vcを生
成する加算部8と、掃引電圧Vsの値を記憶するメモリ
部9とを備えている。
The earth station receiving apparatus of the present invention oscillates at a frequency corresponding to the oscillation control voltage Vc and outputs an oscillation signal Sv, an oscillation signal Sv and an intermediate frequency signal S2. And the phase difference voltage Vp
, A synchronization detection unit 6 that detects when a predetermined signal is detected from the demodulated signal S3 to synchronize with the oscillation signal Sv, and a sweep voltage Vs that sweeps the oscillation frequency of the voltage control oscillation unit 4. , A summation unit 8 that adds the phase difference voltage Vp and the sweep voltage Vs to generate the oscillation control voltage Vc, and a memory unit 9 that stores the value of the sweep voltage Vs. .

【0009】次に動作を説明する。Next, the operation will be described.

【0010】まず、動作開始時、制御部10へモード選
択信号Smを供給して初期モードを指定する。制御部1
0は、局部発振部2へ制御信号C1を送出し、通信衛星
からの電波の内、システムパイロット信号に対応する局
発信号を指定する。同時に、掃引制御部7へ制御信号C
2を送出して広域掃引モードを指定する。掃引制御部7
は、掃引電圧Vsを大きく変化させて、VCO4の発振
信号Svの周波数が通信衛星本体の周波数変動の最大値
を超えて掃引するように制御する。復調部3は、発振信
号Svに応じて中間周波信号S2を復調する。同期検知
部6は、システムパイロット信号を検出して発振信号S
vと同期したときを検知し、同期検知信号Ssを掃引制
御部7へ送出する。同期検知信号Ssを受けた掃引制御
部7は、掃引を停止すると共に、掃引停止時の掃引電圧
Vsの値をメモリ部9に記憶させる。
First, at the start of operation, a mode selection signal Sm is supplied to the control unit 10 to designate an initial mode. Control unit 1
0 transmits the control signal C1 to the local oscillating unit 2 and designates a local oscillation signal corresponding to the system pilot signal among radio waves from the communication satellite. At the same time, the control signal C is sent to the sweep control unit 7.
Send 2 to specify wide-area sweep mode. Sweep controller 7
Controls the sweep voltage Vs so that the frequency of the oscillation signal Sv of the VCO 4 sweeps beyond the maximum value of the frequency variation of the communication satellite body. The demodulation unit 3 demodulates the intermediate frequency signal S2 according to the oscillation signal Sv. The synchronization detector 6 detects the system pilot signal and outputs the oscillation signal S
The synchronization detection signal Ss is sent to the sweep control unit 7 when synchronization with v is detected. Upon receiving the synchronization detection signal Ss, the sweep control unit 7 stops the sweep, and causes the memory unit 9 to store the value of the sweep voltage Vs at the time when the sweep is stopped.

【0011】次に、モード選択信号Smにより制御部1
0に運用モードを指定する。制御部10は、制御信号C
2により掃引制御部7に狭域掃引モードを指定する。掃
引制御部7は、メモリ部9に記憶させていた掃引停止時
の掃引電圧Vsの値を読出し、この電圧値を中心に掃引
電圧Vsを小さく変化させる。復調部3は、発振信号S
vに応じて中間周波信号S2を復調する。同期検知部6
は、復調信号S3に含まれている希望信号を検出して発
振信号Svと同期したときにこれを検知し、同期検知信
号Ssを掃引制御部7へ送出する。掃引制御部7は、同
期検知信号Ssを受けた掃引を停止する。
Next, the control unit 1 is controlled by the mode selection signal Sm.
Specify the operation mode as 0. The control unit 10 controls the control signal C
2 specifies the narrow-range sweep mode to the sweep control unit 7. The sweep control unit 7 reads the value of the sweep voltage Vs at the time of the stop of the sweep stored in the memory unit 9 and changes the sweep voltage Vs to a small value around the voltage value. The demodulation unit 3 outputs the oscillation signal S
The intermediate frequency signal S2 is demodulated according to v. Synchronization detector 6
Detects the desired signal included in the demodulated signal S3 and detects when it synchronizes with the oscillation signal Sv, and sends out a synchronization detection signal Ss to the sweep control unit 7. The sweep control unit 7 stops the sweep receiving the synchronization detection signal Ss.

【0012】このようにすることにより、運用モードに
おける掃引範囲は、システムパイロット信号を送信する
基準局の送信周波数と、伝送信号を送信する地球局の送
信周波数との差以上であれば同期可能であり、通常の通
信衛星本体の周波数変動に比して遥かに小さくできる。
従って、伝送信号の間隔を広げなくても隣接する伝送信
号に誤同期することはない。
By doing so, the sweep range in the operation mode can be synchronized if it is equal to or greater than the difference between the transmission frequency of the reference station transmitting the system pilot signal and the transmission frequency of the earth station transmitting the transmission signal. It can be made much smaller than the frequency fluctuation of the normal communication satellite body.
Therefore, there is no possibility of erroneous synchronization with an adjacent transmission signal even if the interval between transmission signals is not widened.

【0013】なお、本実施例では、外部からモード選択
信号を供給しているが、電源投入時に自動的に初期モー
ドとなり、同期がとれたら運用モードに切替わるように
してもよい。
In this embodiment, the mode selection signal is supplied from the outside. However, the mode may be automatically switched to the initial mode when the power is turned on, and the operation mode may be switched to the operation mode when synchronization is established.

【0014】[0014]

【発明の効果】以上説明したように本発明によれば、動
作開始時は、掃引制御部を広域掃引モードにして掃引電
圧Vsを大きく変化させ、VCOの発振信号の周波数を
通信衛星本体の周波数変動の最大値を超えて掃引させ、
システムパイロット信号と同期したときに掃引を停止さ
せて、掃引停止時の掃引電圧の値をメモリに記憶させ、
その後、掃引制御部を運用モードにして、メモリに記憶
させていた掃引停止時の掃引電圧の値を読出し、この電
圧値を中心に掃引電圧を小さく変化させて、希望信号を
検出したときに掃引を停止させることにより、運用モー
ドにおける掃引範囲を小さくできるので、特に専用のA
FC回路を設けなくても、また伝送信号の間隔を広げな
くても、隣接する伝送信号に誤同期することなく通信衛
星本体の周波数変動に対応できる。
As described above, according to the present invention, when the operation is started, the sweep control unit is set to the wide-area sweep mode to greatly change the sweep voltage Vs, and the frequency of the oscillation signal of the VCO is changed to the frequency of the communication satellite body. Sweep beyond the maximum value of the fluctuation,
Stop the sweep when synchronized with the system pilot signal, store the value of the sweep voltage at the time of the sweep stop in the memory,
After that, the sweep control unit is set to the operation mode, the value of the sweep voltage at the time of the stop of the sweep stored in the memory is read out, and the sweep voltage is changed small around this voltage value, and the sweep is performed when a desired signal is detected. , The sweep range in the operation mode can be reduced.
Even if the FC circuit is not provided and the interval between the transmission signals is not widened, it is possible to cope with the frequency fluctuation of the communication satellite body without erroneous synchronization with the adjacent transmission signal.

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

【図1】本発明の一実施例を示すブロック図である。FIG. 1 is a block diagram showing one embodiment of the present invention.

【符号の説明】[Explanation of symbols]

1 周波数変換部 3 復調部 4 電圧制御発振部(VCO) 5 位相比較部 6 同期検知部 7 掃引制御部 8 加算部 9 メモリ部 S1 受信信号 S2 中間周波信号 S3 復調信号 Ss 同期検知信号 Sv 発振信号 Vc 発振制御電圧 Vp 位相差電圧 Vs 掃引電圧 DESCRIPTION OF SYMBOLS 1 Frequency conversion part 3 Demodulation part 4 Voltage control oscillation part (VCO) 5 Phase comparison part 6 Synchronization detection part 7 Sweep control part 8 Addition part 9 Memory part S1 Reception signal S2 Intermediate frequency signal S3 Demodulation signal Ss Synchronization detection signal Sv Oscillation signal Vc Oscillation control voltage Vp Phase difference voltage Vs Sweep voltage

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 受信信号を中間周波信号に変換する周波
数変換部と、発振制御電圧に応じた周波数の発振信号を
出力する電圧制御発振部と、前記発振信号に応じて前記
中間周波信号を復調して復調信号を出力する復調部と、
前記発振信号と前記中間周波信号との位相差を検出して
位相差電圧を生成する位相比較部と、前記電圧制御発振
部の発振周波数を掃引するために所定の電圧範囲で変化
する掃引電圧を生成する掃引制御部と、前記位相差電圧
と前記掃引電圧とを加算して前記発振制御電圧を生成す
る加算部と、前記復調信号の所定の信号と前記発振信号
とが同期したときを検知する同期検知部と、前記掃引電
圧の値を記憶するメモリ部とを備えることを特徴とする
地球局受信装置。
A frequency converter for converting a received signal into an intermediate frequency signal; a voltage controlled oscillator for outputting an oscillation signal having a frequency corresponding to an oscillation control voltage; and a demodulator for demodulating the intermediate frequency signal according to the oscillation signal. A demodulation unit for outputting a demodulated signal
A phase comparison unit that detects a phase difference between the oscillation signal and the intermediate frequency signal to generate a phase difference voltage, and a sweep voltage that changes in a predetermined voltage range to sweep the oscillation frequency of the voltage control oscillation unit. A sweep control unit for generating, an adding unit for adding the phase difference voltage and the sweep voltage to generate the oscillation control voltage, and detecting when a predetermined signal of the demodulated signal is synchronized with the oscillation signal. An earth station receiving device comprising: a synchronization detecting unit; and a memory unit for storing the value of the sweep voltage.
【請求項2】 前記掃引制御部は、動作開始時、前記発
振信号が前記通信衛星側の周波数変動の最大値を超えて
掃引するように前記掃引電圧を大きく変化させ、また前
記同期検知部が、基準局から送出されたシステムパイロ
ット信号と前記発振信号との同期を検知したときに掃引
を停止し、更に掃引停止時の掃引電圧の値を前記メモリ
部に記憶させ、その後、前記メモリ部に記憶させた前記
掃引停止時の掃引電圧の値を中心に小さく前記掃引電圧
を変化させ、前記同期検知部が、希望信号と前記発振信
号との同期を検知したときに掃引を停止することを特徴
とする請求項1記載の地球局受信装置。
2. The method according to claim 1, wherein the sweep control section changes the sweep voltage so that the oscillation signal sweeps beyond a maximum value of a frequency variation on the communication satellite side when the operation is started. When the synchronization between the system pilot signal transmitted from the reference station and the oscillation signal is detected, the sweep is stopped, and the value of the sweep voltage at the time of stopping the sweep is stored in the memory unit. The sweep voltage is changed to be small around the value of the sweep voltage at the time of stopping the sweep, and the synchronization detection unit stops the sweep when the synchronization between the desired signal and the oscillation signal is detected. The earth station receiving device according to claim 1.
JP3264385A 1991-10-14 1991-10-14 Earth station receiver Expired - Lifetime JP3042083B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3264385A JP3042083B2 (en) 1991-10-14 1991-10-14 Earth station receiver

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3264385A JP3042083B2 (en) 1991-10-14 1991-10-14 Earth station receiver

Publications (2)

Publication Number Publication Date
JPH05110484A JPH05110484A (en) 1993-04-30
JP3042083B2 true JP3042083B2 (en) 2000-05-15

Family

ID=17402424

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3264385A Expired - Lifetime JP3042083B2 (en) 1991-10-14 1991-10-14 Earth station receiver

Country Status (1)

Country Link
JP (1) JP3042083B2 (en)

Also Published As

Publication number Publication date
JPH05110484A (en) 1993-04-30

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