JPH05206910A - Satellite acquisition system for satellite communication earth station - Google Patents

Satellite acquisition system for satellite communication earth station

Info

Publication number
JPH05206910A
JPH05206910A JP1349192A JP1349192A JPH05206910A JP H05206910 A JPH05206910 A JP H05206910A JP 1349192 A JP1349192 A JP 1349192A JP 1349192 A JP1349192 A JP 1349192A JP H05206910 A JPH05206910 A JP H05206910A
Authority
JP
Japan
Prior art keywords
satellite
code
antenna
receiver
scpc
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
JP1349192A
Other languages
Japanese (ja)
Other versions
JP2836335B2 (en
Inventor
Hiroaki Adachi
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 JP4013491A priority Critical patent/JP2836335B2/en
Publication of JPH05206910A publication Critical patent/JPH05206910A/en
Application granted granted Critical
Publication of JP2836335B2 publication Critical patent/JP2836335B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE:To accurately acquire a communication satellite in a simple addition circuit. CONSTITUTION:A control circuit 12 discriminates whether AGC voltage 10 which a receiver 6 generates exceeds prescribed voltage or not. An ID code is detected from a demodulation signal 8 which the receiver 5 outputs and it is discriminated whether the ID code coincides with a previously decided ID code or not. An antenna 1 is adjusted as follows. First, a reception frequency is set so that an SCPC carrier signal transmitted from the satellite can be received in the receiver 6. Then, the antenna 1 is adjusted and it is set to receive the signal in a regular level based on the discriminated result of AGC voltage 10 by the control circuit 12. Then, the discriminated result of the 1D code by the control circuit 12 is monitored. When the ID code detected by a demodulation signal 8 coincides with the previously decided ID code, it is judged that the direction of the antenna 1 is correctly set. When it does not coincide in evidence that the satellite different from the prescribed satellite is acquired, so adjustment is tried.

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、衛星通信地球局のアン
テナの方向を調整して衛星を捕捉するための方式に関す
るものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a system for adjusting the direction of an antenna of a satellite communication earth station to acquire a satellite.

【0002】[0002]

【従来の技術】SCPC(Single Channel Per Carrie
r)方式によって音声またはデータ信号を伝送する従来
の衛星通信地球局の一例を図2に示す。送信信号9はS
CPC用送信機4および高周波増幅器3を通じてフィー
ダ2に供給され、そしてアンテナ1を通じて通信衛星に
送信される。一方、通信衛星からの信号はアンテナ1で
受信され、フィーダ2および低雑音増幅器5を通じてS
CPC用受信機6に入力され、受信機6はSCPC方式
のキャリア信号、すなわちSCPCキャリア信号の復調
信号8を出力する。
2. Description of the Related Art SCPC (Single Channel Per Carrie)
FIG. 2 shows an example of a conventional satellite communication earth station for transmitting voice or data signals by the r) method. Transmission signal 9 is S
It is supplied to the feeder 2 through the CPC transmitter 4 and the high frequency amplifier 3, and then transmitted to the communication satellite through the antenna 1. On the other hand, the signal from the communication satellite is received by the antenna 1 and passed through the feeder 2 and the low noise amplifier 5 to S
The signal is input to the CPC receiver 6, and the receiver 6 outputs a carrier signal of the SCPC system, that is, a demodulated signal 8 of the SCPC carrier signal.

【0003】ところで、このような地球局により衛星通
信を行うためにはアンテナ1の方向を正確に所要の衛星
に向ける必要がある。そこで従来は、スペアナ7によっ
て受信信号を観測し、アンテナの方向を調整していた。
SCPCキャリア信号のレベルはTV信号と比較して低
く、また狭帯域であるため、一般にスペアナ7は増幅器
5の出力に接続し、受信信号内で比較的レベルの高いT
V信号などを観測してアンテナを調整する。
By the way, in order to perform satellite communication by such an earth station, it is necessary to orient the direction of the antenna 1 to a required satellite accurately. Therefore, in the past, the received signal was observed by the spectrum analyzer 7 and the direction of the antenna was adjusted.
Since the level of the SCPC carrier signal is lower than that of the TV signal and has a narrow band, the spectrum analyzer 7 is generally connected to the output of the amplifier 5 and has a relatively high level in the received signal.
Adjust the antenna by observing V signals.

【0004】また、地球局が可搬局であり、軽量性が要
求されるためスペアナが利用できない場合には、図3の
ようにスペアナの変りにメータ回路11が用いられ、受
信機6がSCPC用キャリ信号を受信して発生するAG
C電圧10をメータ回路11のメータの振れによって観
測し、そのAGC電圧が表す受信レベルが最大となるよ
うにアンテナの方向を調整していた。なお、受信機6は
具体的には、SCPC方式において周波数安定化のため
の基準信号となるパイロット信号によりAGC電圧を発
生する。
Further, when the earth station is a portable station and lightweight is required and therefore the spectrum analyzer cannot be used, the meter circuit 11 is used instead of the spectrum analyzer as shown in FIG. Generated by receiving a carry signal for
The C voltage 10 is observed by the swing of the meter of the meter circuit 11, and the direction of the antenna is adjusted so that the reception level represented by the AGC voltage becomes maximum. The receiver 6 specifically generates an AGC voltage by a pilot signal that serves as a reference signal for frequency stabilization in the SCPC method.

【0005】[0005]

【発明が解決しようとする課題】しかし、最近では多数
の通信衛星が打ち上げられ、各衛星間の間隔はアジマス
方向で数度程度に狭まっている。従って、スペアナを利
用できない可搬局の場合には、このように近接して配置
されている衛星を正しく捕捉することは難しい。
However, recently, a large number of communication satellites have been launched, and the distance between the satellites is narrowed to a few degrees in the azimuth direction. Therefore, in the case of a mobile station in which the spectrum analyzer cannot be used, it is difficult to correctly acquire satellites arranged in such a close proximity.

【0006】特に、同一周波数のSCPC信号を利用す
る複数の衛星が近接して配置されている場合には、受信
レベルしか観測できない可搬局では誤って別の衛星を捕
捉してしまう可能性が高い。例えば、現用の衛星と予備
の衛星とが配置されてい場合には、トランスポンダーは
同一の周波数に設定されていることが多く、上記パイロ
ット信号も同一の周波数に設定されている。従ってその
ような場合、所要の衛星を正しく捕捉することは極めて
困難である。
Particularly, when a plurality of satellites using the SCPC signal of the same frequency are arranged close to each other, there is a possibility that a portable station which can observe only the reception level may erroneously capture another satellite. high. For example, when an active satellite and a spare satellite are arranged, the transponder is often set to the same frequency, and the pilot signal is also set to the same frequency. Therefore, in such a case, it is extremely difficult to correctly acquire the required satellite.

【0007】本発明の目的は、このような問題を解決
し、簡単な回路を追加するのみで、通信衛星を正しく捕
捉できるようにする衛星通信地球局の衛星捕捉方式を提
供することにある。
An object of the present invention is to solve the above problems and to provide a satellite acquisition system for a satellite communication earth station which can correctly acquire a communication satellite by only adding a simple circuit.

【0008】[0008]

【課題を解決するための手段】本発明は、衛星通信地球
局のアンテナの方向を調整して衛星を捕捉するための方
式において、SCPCキャリア信号の復調信号を出力
し、かつAGC電圧を発生するSCPC用受信機と、こ
のSCPC用受信機が発生した前記AGC電圧により、
受信レベルを判別するレベル判別手段と、前記SCPC
用受信機が出力する前記復調信号よりIDコードを取得
し、そのIDコードを所定のIDコードと比較してそれ
らが一致するか否かを判別するコード判別手段とを前記
衛星通信地球局に設けることを特徴とする。
The present invention outputs a demodulated signal of an SCPC carrier signal and generates an AGC voltage in a system for acquiring the satellite by adjusting the direction of the antenna of a satellite communication earth station. By the receiver for SCPC and the AGC voltage generated by the receiver for SCPC,
Level discriminating means for discriminating a reception level, and the SCPC
The satellite communication earth station is provided with a code discriminating means for obtaining an ID code from the demodulated signal output from the receiver for radio and comparing the ID code with a predetermined ID code to discriminate whether or not they match. It is characterized by

【0009】[0009]

【作用】例えば現用と予備の衛星が存在し、それらのト
ランスポンダーが同一の周波数に設定されている場合で
もSCPCキャリア信号は、現用と予備とでは異なるI
Dコードで変調されている。従って、本発明の衛星捕捉
方式にもとづく衛星通信地球局では、次のようにしてア
ンテナの方向を正しく調整できる。すなわち、まずSC
PC用受信機において衛星から送られてくるSCPCキ
ャリア信号を受信できるように、受信周波数をキャリ信
号の周波数に設定する。次に、アンテナを調整し、レベ
ル判別手段によるAGC電圧の判別結果にもとづき正規
のレベルで受信できるようにする。その後、コード判別
手段によるIDコードの判別結果をモニタし、復調信号
より検出したIDコードが所定のIDコードに一致して
いる場合には、アンテナの方向は正しく設定されている
と判断する。一方、IDコードが一致していない場合に
は、所要の衛星とは別の衛星を捕捉していることにな
り、アンテナの調整をやり直す。
For example, even when a working satellite and a spare satellite are present and their transponders are set to the same frequency, the SCPC carrier signal is different between the working and the spare I.
It is modulated with the D code. Therefore, in the satellite communication earth station based on the satellite acquisition system of the present invention, the direction of the antenna can be adjusted correctly as follows. That is, first SC
The reception frequency is set to the frequency of the carry signal so that the PC receiver can receive the SCPC carrier signal transmitted from the satellite. Next, the antenna is adjusted so that the signal can be received at a normal level based on the result of the AGC voltage discrimination by the level discriminating means. After that, the result of ID code discrimination by the code discriminating means is monitored, and when the ID code detected from the demodulated signal matches a predetermined ID code, it is determined that the direction of the antenna is set correctly. On the other hand, if the ID codes do not match, it means that a satellite different from the required satellite has been captured, and the antenna adjustment is performed again.

【0010】レベル判別手段は単に電圧のレベルを判別
し、コード判別手段は単にIDコードを判別するだけで
あるから、それらは例えばCPUなどを用いて容易に実
現できる。従って、本発明により簡単な回路を追加する
のみで、通信衛星を正しく捕捉することが可能となる。
本発明は特に軽量性が要求される可搬局に対して有効で
ある。
Since the level discriminating means merely discriminates the voltage level and the code discriminating means merely discriminates the ID code, they can be easily realized by using, for example, a CPU. Therefore, according to the present invention, the communication satellite can be correctly captured only by adding a simple circuit.
The present invention is particularly effective for a portable station that needs to be lightweight.

【0011】[0011]

【実施例】次に本発明の実施例について図面を参照して
説明する。図1に本発明の衛星捕捉方式にもとづく衛星
通信地球局の一例を示す。この地球局の基本構成は図
2,3に示した地球局と同一であり、アンテナ1、フィ
ーダ2、高周波増幅器3、SCPC用送信機4、低雑音
増幅器5、ならびにSCPC用受信機6を備えている。
そして、送信信号9はSCPC用送信機4および高周波
増幅器3を通じてフィーダ2に供給され、アンテナ1を
通じて通信衛星に送信される。一方、通信衛星からの信
号はアンテナ1で受信され、フィーダ2および低雑音増
幅器5を通じてSCPC用受信機6に入力され、受信機
6はSCPCキャリア信号の復調信号8を出力し、また
受信レベルに対応するAGC電圧10を発生する。
Embodiments of the present invention will now be described with reference to the drawings. FIG. 1 shows an example of a satellite communication earth station based on the satellite acquisition system of the present invention. The basic configuration of this earth station is the same as the earth station shown in FIGS. 2 and 3, and is provided with an antenna 1, a feeder 2, a high frequency amplifier 3, a transmitter 4 for SCPC, a low noise amplifier 5 and a receiver 6 for SCPC. ing.
Then, the transmission signal 9 is supplied to the feeder 2 through the SCPC transmitter 4 and the high frequency amplifier 3, and is transmitted to the communication satellite through the antenna 1. On the other hand, the signal from the communication satellite is received by the antenna 1, is input to the receiver 6 for the SCPC through the feeder 2 and the low noise amplifier 5, and the receiver 6 outputs the demodulated signal 8 of the SCPC carrier signal, and the reception level is changed. Generate a corresponding AGC voltage 10.

【0012】この地球局はさらに制御回路12を備えて
いる。制御回路12は2つの機能を備えており、まず受
信機6が発生するAGC電圧10が所定の電圧を越える
か否かを判別する。制御回路12はまた、受信機6が出
力する復調信号8よりIDコードを検出し、それが予め
決められたIDコードに一致するか否かを判別する。
The earth station further includes a control circuit 12. The control circuit 12 has two functions. First, it is determined whether the AGC voltage 10 generated by the receiver 6 exceeds a predetermined voltage. The control circuit 12 also detects the ID code from the demodulated signal 8 output from the receiver 6 and determines whether or not it matches the predetermined ID code.

【0013】この地球局ではアンテナ1の調整は次のよ
うに行う。まず、受信機6において衛星から送られてく
るSCPCキャリア信号を受信できるように、受信周波
数をキャリ信号の周波数に設定する。次に、アンテナ1
を調整し、制御回路12によるAGC電圧10の判別結
果にもとづき正規のレベルで受信できるようにする。そ
の後、制御回路12によるIDコードの判別結果をモニ
タし、復調信号8より検出したIDコードが予め決めら
れたIDコードに一致している場合には、アンテナ1の
方向は正しく設定されていると判断する。一方、IDコ
ードが一致していない場合には、所要の衛星とは別の衛
星を捕捉していることになり、アンテナ1の調整をやり
直す。
In this earth station, the antenna 1 is adjusted as follows. First, the reception frequency is set to the frequency of the carry signal so that the receiver 6 can receive the SCPC carrier signal sent from the satellite. Next, antenna 1
Is adjusted so that the control circuit 12 can receive the signal at a normal level based on the determination result of the AGC voltage 10. After that, the result of the ID code discrimination by the control circuit 12 is monitored, and if the ID code detected from the demodulated signal 8 matches the predetermined ID code, the direction of the antenna 1 is set correctly. to decide. On the other hand, if the ID codes do not match, it means that a satellite different from the required satellite is captured, and the antenna 1 is readjusted.

【0014】なお、制御回路12は、AGC電圧および
IDコードの判断を行うのみであるから、CPUなどを
用いて容易に実現可能である。
Since the control circuit 12 only judges the AGC voltage and the ID code, it can be easily realized by using a CPU or the like.

【0015】[0015]

【発明の効果】本発明の衛星捕捉方式にもとづく衛星通
信地球局では、次のようにしてアンテナの方向を調整す
る。すなわち、まずSCPC用受信機において衛星から
送られてくるSCPCキャリア信号を受信できるよう
に、受信周波数をキャリ信号の周波数に設定する。次
に、アンテナを調整し、レベル判別手段によるAGC電
圧の判別結果にもとづき正規のレベルで受信できるよう
にする。その後、コード判別手段によるIDコードの判
別結果をモニタし、復調信号より検出したIDコードが
所定のIDコードに一致している場合には、アンテナの
方向は正しく設定されていると判断する。一方、IDコ
ードが一致していない場合には、所要の衛星とは別の衛
星を捕捉していることになり、アンテナの調整をやり直
す。
In the satellite communication earth station based on the satellite acquisition system of the present invention, the direction of the antenna is adjusted as follows. That is, first, the reception frequency is set to the frequency of the carry signal so that the SCPC receiver can receive the SCPC carrier signal sent from the satellite. Next, the antenna is adjusted so that the signal can be received at a normal level based on the result of the AGC voltage discrimination by the level discriminating means. After that, the result of ID code discrimination by the code discriminating means is monitored, and when the ID code detected from the demodulated signal matches a predetermined ID code, it is determined that the direction of the antenna is set correctly. On the other hand, if the ID codes do not match, it means that a satellite different from the required satellite has been captured, and the antenna adjustment is performed again.

【0016】このように、AGC電圧のレベルだけでな
く、IDコードも参照するので、複数の衛星が近接して
配置されている場合でも、あるいはさらに同一の周波数
が用いられている場合でも、通信衛星を正しく捕捉する
ことができる。
As described above, not only the AGC voltage level but also the ID code is referred to. Therefore, even when a plurality of satellites are arranged close to each other or even when the same frequency is used, communication is performed. The satellite can be captured correctly.

【0017】レベル判別手段は単に電圧のレベルを判別
し、コード判別手段は単にIDコードを判別するだけで
あるから、それらは例えばCPUなどを用いて容易に実
現できる。従って、本発明により簡単な回路を追加する
のみで、通信衛星を正しく捕捉することが可能となる。
本発明は特に軽量性が要求される可搬局に対して有効で
ある。
Since the level discriminating means merely discriminates the voltage level and the code discriminating means merely discriminates the ID code, they can be easily realized by using, for example, a CPU. Therefore, according to the present invention, the communication satellite can be correctly captured only by adding a simple circuit.
The present invention is particularly effective for a portable station that needs to be lightweight.

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

【図1】本発明の衛星捕捉方式にもとづく衛星通信地球
局の一例を示すブロック図である。
FIG. 1 is a block diagram showing an example of a satellite communication earth station based on a satellite acquisition system of the present invention.

【図2】従来の衛星捕捉方式にもとづく衛星通信地球局
の一例を示すブロック図である。
FIG. 2 is a block diagram showing an example of a satellite communication earth station based on a conventional satellite acquisition system.

【図3】従来の衛星捕捉方式にもとづく衛星通信地球局
の他の例を示すブロック図である。
FIG. 3 is a block diagram showing another example of a satellite communication earth station based on a conventional satellite acquisition system.

【符号の説明】[Explanation of symbols]

1 アンテナ 2 フィーダ 3 高周波増幅器 4 SCPC用送信機 5 低雑音増幅器 6 SCPC用受信機 12 制御回路 1 Antenna 2 Feeder 3 High Frequency Amplifier 4 Transmitter for SCPC 5 Low Noise Amplifier 6 Receiver for SCPC 12 Control Circuit

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】衛星通信地球局のアンテナの方向を調整し
て衛星を捕捉するための方式において、 SCPCキャリア信号の復調信号を出力し、かつAGC
電圧を発生するSCPC用受信機と、 このSCPC用受信機が発生した前記AGC電圧によ
り、受信レベルを判別するレベル判別手段と、 前記SCPC用受信機が出力する前記復調信号よりID
コードを取得し、そのIDコードを所定のIDコードと
比較してそれらが一致するか否かを判別するコード判別
手段とを前記衛星通信地球局に設けることを特徴とする
衛星通信地球局の衛星捕捉方式。
1. A system for adjusting a direction of an antenna of a satellite communication earth station to capture a satellite, wherein a demodulated signal of an SCPC carrier signal is output and AGC is performed.
A receiver for SCPC that generates a voltage, a level discriminating unit that discriminates a reception level by the AGC voltage generated by the receiver for SCPC, and an ID based on the demodulated signal output by the receiver for SCPC.
A satellite of the satellite communication earth station, characterized in that the satellite communication earth station is provided with code judging means for obtaining a code and comparing the ID code with a predetermined ID code to judge whether or not they match. Capture method.
JP4013491A 1992-01-29 1992-01-29 Satellite acquisition method of satellite communication earth station Expired - Fee Related JP2836335B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4013491A JP2836335B2 (en) 1992-01-29 1992-01-29 Satellite acquisition method of satellite communication earth station

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4013491A JP2836335B2 (en) 1992-01-29 1992-01-29 Satellite acquisition method of satellite communication earth station

Publications (2)

Publication Number Publication Date
JPH05206910A true JPH05206910A (en) 1993-08-13
JP2836335B2 JP2836335B2 (en) 1998-12-14

Family

ID=11834591

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4013491A Expired - Fee Related JP2836335B2 (en) 1992-01-29 1992-01-29 Satellite acquisition method of satellite communication earth station

Country Status (1)

Country Link
JP (1) JP2836335B2 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54129914A (en) * 1978-03-31 1979-10-08 Nec Corp Tracking receiver for scpc antenna
JPS57186849A (en) * 1981-05-13 1982-11-17 Nec Corp Time division multiplex signal communication system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54129914A (en) * 1978-03-31 1979-10-08 Nec Corp Tracking receiver for scpc antenna
JPS57186849A (en) * 1981-05-13 1982-11-17 Nec Corp Time division multiplex signal communication system

Also Published As

Publication number Publication date
JP2836335B2 (en) 1998-12-14

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