JP3033176B2 - AFC device for satellite communication earth station - Google Patents

AFC device for satellite communication earth station

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Publication number
JP3033176B2
JP3033176B2 JP28223690A JP28223690A JP3033176B2 JP 3033176 B2 JP3033176 B2 JP 3033176B2 JP 28223690 A JP28223690 A JP 28223690A JP 28223690 A JP28223690 A JP 28223690A JP 3033176 B2 JP3033176 B2 JP 3033176B2
Authority
JP
Japan
Prior art keywords
frequency
satellite
pilot signal
time
signal
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
JP28223690A
Other languages
Japanese (ja)
Other versions
JPH04156728A (en
Inventor
弘美 下田
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
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Priority to JP28223690A priority Critical patent/JP3033176B2/en
Publication of JPH04156728A publication Critical patent/JPH04156728A/en
Application granted granted Critical
Publication of JP3033176B2 publication Critical patent/JP3033176B2/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、衛星通信地球局用AFC装置に関し、特に移
動体との衛星通信を行う無線装置に使用される衛星通信
地球局用AFC装置に関する。
Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an AFC device for a satellite communication earth station, and more particularly to an AFC device for a satellite communication earth station used for a wireless device for performing satellite communication with a mobile object. .

〔従来の技術〕[Conventional technology]

一般に地球局と移動体とが衛星を介して通信を行う場
合の移動体衛星通信システムにおける送信周波数補正手
段を第3図のシステム構成図および第4図に示す地球局
21に備えられている送信装置の送信周波数補正部25によ
り説明する。通常、地球局21と衛星23間で通信を行う場
合に、静止衛星であっても衛星軌道が約24時間を一周期
とする日変化があるので、ドップラシフトによる周波数
誤差がある。この周波数誤差の補正は、地球上の基準局
24から衛星経由送信される基準パイロット信号を地球局
21が受信して送信周波数の補正を行っている。地球局21
の送信装置内に備えられた送信周波数補正部25(第4
図)は、入力端子26Aから前述の基準パイロット信号を
有する受信信号を受け、受信周波数変換装置26で基準パ
イロット信号を復調する。AFC装置27はこの基準パイロ
ット信号をもとに衛星23に送出する送信信号の周波数に
AFCをかけるべくドップラシフト周波数の演算等を行い
周波数補正信号を作成する。送信周波数変換装置28はこ
の周波数補正信号を受け、送信局部発振器の発振周波数
を補正して出力端子からあらかじめドップラ補正等を行
った正確な送信信号を送出する。第3図にもどり、この
送信信号は衛星23を経由して航空機等の移動体22に送出
される。ここで衛星23と移動体22間の伝送周波数でも当
然大きいドップラシフトを生ずる。この大きいドップラ
シフトに比して地球局21と衛星23間のドップラシフトは
小さいが、衛星と航空機間の大きいドップラシフトの補
正に対する負担を軽減するために送信周波数補正部25に
よりあらかじめ補正している。
Generally, a transmission frequency correcting means in a mobile satellite communication system in the case where an earth station and a mobile unit communicate with each other via a satellite is a system configuration diagram shown in FIG. 3 and an earth station shown in FIG.
The transmission frequency correction unit 25 of the transmission device provided in 21 will be described. Normally, when communication is performed between the earth station 21 and the satellite 23, even if it is a geostationary satellite, since the satellite orbit has a daily change of about 24 hours, there is a frequency error due to the Doppler shift. Correction of this frequency error is performed by a reference station on the earth.
The reference pilot signal transmitted via satellite from 24
21 receives and corrects the transmission frequency. Earth station 21
The transmission frequency correction unit 25 (4th
3) receives a received signal having the above-mentioned reference pilot signal from an input terminal 26A, and demodulates the reference pilot signal by a reception frequency conversion device 26. The AFC device 27 determines the frequency of the transmission signal to be transmitted to the satellite 23 based on the reference pilot signal.
To apply AFC, calculate the Doppler shift frequency and create a frequency correction signal. The transmission frequency conversion device 28 receives the frequency correction signal, corrects the oscillation frequency of the transmission local oscillator, and sends out an accurate transmission signal that has been subjected to Doppler correction or the like in advance from the output terminal. Returning to FIG. 3, this transmission signal is transmitted to a moving body 22 such as an aircraft via a satellite 23. Here, the transmission frequency between the satellite 23 and the mobile unit 22 naturally causes a large Doppler shift. Although the Doppler shift between the earth station 21 and the satellite 23 is small compared to the large Doppler shift, the Doppler shift is corrected in advance by the transmission frequency correction unit 25 in order to reduce the burden on the correction of the large Doppler shift between the satellite and the aircraft. .

従来、この種のAFC装置27としては、第2図に示すよ
うに、基準パイロット信号を入力する入力端子5A,この
基準パイロット信号をもとに内蔵する電圧制御発振器
(VCO)に位相同期をかけ、S/Nのよい基準信号を作成す
るAFC回路2,この基準信号の周波数計数用と、後述する
送信信号用の電圧制御クリスタル発振器(VCXO)6の周
波数計数も行う周波数カウンタ2,AFC回路5の基準信号
をもとに基準局及び地球局の緯度,経度と衛星の軌道傾
斜角から衛星のドップラシフトと衛星中継器のローカル
発振器の変動を算出し、地球局と衛星間の周波数誤差を
あらかじめ付加するための補正信号を送出するCPU3,送
信信号の局部発振信号の原振となり、前述の補正信号で
補正された周波数の信号を発振するVCXO6,VCXO6の出力
を第4図の送信周波数変換装置28に送出する出力端子7A
を有する分岐回路7,なお分岐回路7はこの補正周波数計
数のために周波数カウンタ2にも分岐している。前述の
基準パイロット信号の周波数のデータを所定の時間間隔
で少なくとも24時間記憶して行く記憶回路4から構成さ
れていた。
Conventionally, as this type of AFC device 27, as shown in FIG. 2, an input terminal 5A for inputting a reference pilot signal and a built-in voltage controlled oscillator (VCO) based on the reference pilot signal are phase-locked. AFC circuit 2 for generating a reference signal having a good S / N ratio, a frequency counter 2 for counting the frequency of this reference signal, and also for counting the frequency of a voltage controlled crystal oscillator (VCXO) 6 for a transmission signal described later, AFC circuit 5 The Doppler shift of the satellite and the fluctuation of the local oscillator of the satellite transponder are calculated from the latitude and longitude of the reference station and the earth station and the orbit inclination of the satellite based on the reference signal of, and the frequency error between the earth station and the satellite is added in advance. The CPU 3 for transmitting a correction signal for performing the correction, the source of the local oscillation signal of the transmission signal, and the output of the VCXO 6 and the VCXO 6 for oscillating the signal of the frequency corrected by the above-described correction signal are transmitted to the transmission frequency converter 28 shown in FIG. Send out to Force terminal 7A
, Which also branches to the frequency counter 2 for counting the correction frequency. The storage circuit 4 stores the data of the frequency of the above-mentioned reference pilot signal at predetermined time intervals for at least 24 hours.

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

上述した従来の衛星通信地球局用AFC装置では、基準
パイロット信号の周波数誤差のデータを定期的にサンプ
リングし、記憶回路に蓄え24時間分蓄積した後に、衛星
のドップラシフトの周期と衛星中継器とローカル発振器
の変動を算出し、周波数補正を行っているので、一たん
基準パイロット信号に異常が発生したときには、復旧す
るまでサンプリングデータが欠落し、周波数誤差の算出
が行えず、パイロット信号の復旧後も24時間待たなけれ
ばならないという欠点があった。
In the above-mentioned conventional AFC device for a satellite communication earth station, the data of the frequency error of the reference pilot signal is periodically sampled and stored in a storage circuit for 24 hours, and then the Doppler shift period of the satellite and the satellite repeater are used. Since the fluctuation of the local oscillator is calculated and the frequency is corrected, if an error occurs in the reference pilot signal, the sampling data is lost until recovery, the frequency error cannot be calculated, and after the pilot signal is recovered. Had the disadvantage of having to wait 24 hours.

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

本発明の衛星通信地球局用AFC装置は、 衛星通信の基準局から送出される基準パイロット信号を
衛星を経由して受信し、前記基準パイロット信号に基づ
いて位相同期をかけ基準信号を作成する地球局のAFC回
路と、 前記地球局から前記衛星に向けて送信する送信信号を
発生するための電圧制御発振器と、 前記基準信号の周波数および前記送信信号の周波数を
計数する周波数カウンタと、 前記周波数カウンタに接続され、前記基準信号を基に
衛星のドプラーシフトと衛星中継器のローカル発振器の
変動を算出し、前記地球局と衛星間の周波数誤差を予め
付加するための周波数補正データとして前記電圧制御発
振器に送出する処理手段と、 前記周波数補正データを所定の時間間隔で少なくとも
24時間記憶する記憶回路と、 前記基準パイロット信号が受信されなくなってから前
記基準パイロット信号の受信が復旧されるまでの時間を
計数するタイマー回路とを備え、 前記処理手段は、 前記基準パイロット信号が受信されなかった場合に、前
記記憶回路から24時間前に記憶された周波数補正データ
を読み出し前記電圧制御発信器に供給すること、および
前記記憶回路から24時間前に記憶された周波数補正デー
タを読み出した時刻と、前記タイマー回路で計数した時
間を基に前記パイロット信号の復旧後に正規のAFC動作
を開始すべき時刻を決め、正規の周波数補正時刻に切替
えることを特徴とする。
An AFC device for a satellite communication earth station according to the present invention is an earth station for receiving a reference pilot signal transmitted from a reference station for satellite communication via a satellite, performing phase synchronization based on the reference pilot signal, and creating a reference signal. An AFC circuit, a voltage-controlled oscillator for generating a transmission signal transmitted from the earth station to the satellite, a frequency counter for counting the frequency of the reference signal and the frequency of the transmission signal, and the frequency counter Connected, calculates the Doppler shift of the satellite and the variation of the local oscillator of the satellite transponder based on the reference signal, and supplies the voltage-controlled oscillator as frequency correction data for adding a frequency error between the earth station and the satellite in advance. Processing means for transmitting, at least at predetermined time intervals the frequency correction data
A storage circuit for storing for 24 hours, and a timer circuit for counting the time from when the reference pilot signal is no longer received until the reception of the reference pilot signal is restored, wherein the processing means is configured such that the reference pilot signal is If not received, read out the frequency correction data stored 24 hours ago from the storage circuit and supply it to the voltage control transmitter, and read out the frequency correction data stored 24 hours ago from the storage circuit The time when the normal AFC operation is to be started after the restoration of the pilot signal is determined based on the time counted by the timer circuit and the time counted by the timer circuit, and the time is switched to the normal frequency correction time.

〔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 described with reference to the drawings.

第1図は本発明の一実施例のブロック図である。第1
図において第2図の同一の符号は同一の構成と動作を行
う。すなわち、本実施例ではタイマー回路1を追加して
いる。
FIG. 1 is a block diagram of one embodiment of the present invention. First
In the figure, the same reference numerals in FIG. 2 perform the same configuration and operation. That is, in this embodiment, the timer circuit 1 is added.

次に本実施例の動作を説明する。今、基準局24から基
準パイロット信号が何らかの異常で受信できなかった場
合について説明する。前述したように、衛星のドップラ
シフトによる周波数誤差は、約24時間を一周期とするサ
インカーブを取り、その値は、前日と同様に変化する。
また、衛星中継器のローカル発振器の周波数誤差の1日
当たりの変化は、微少であり前日とほぼ同一であること
に着目すると、受信している基準パイロット信号に異常
が発生した場合でも、24時間前の周波数補正データを取
り出してAFC機能を継続する事が可能である。さらに、
受信している基準パイロット信号が復旧するまでの時間
を正確に認識するタイマー回路5を追加することによ
り、前の記憶されている補正データを使用している24時
間ごとの補正時刻から、基準パイロット信号復旧後に開
始される補正時刻への切り換えを正確に行うことができ
る。したがって、長時間のパイロット信号の異常に対応
することができる。
Next, the operation of this embodiment will be described. Now, a case where the reference pilot signal from the reference station 24 cannot be received due to some abnormality will be described. As described above, the frequency error due to the Doppler shift of the satellite takes a sine curve with one cycle of about 24 hours, and the value changes in the same manner as the previous day.
Focusing on the fact that the change in the frequency error of the local oscillator of the satellite repeater per day is very small and almost the same as the previous day, even if the received reference pilot signal has an abnormality, It is possible to take out the frequency correction data and continue the AFC function. further,
By adding a timer circuit 5 that accurately recognizes the time until the received reference pilot signal is restored, the reference pilot signal can be calculated from the correction time every 24 hours using the previously stored correction data. The switching to the correction time started after the signal restoration can be accurately performed. Therefore, it is possible to cope with a long-term abnormality of the pilot signal.

〔発明の効果〕〔The invention's effect〕

以上説明したように本発明は、タイマー回路の追加と
それに伴う制御方法の変更により、受信している基準パ
イロット信号に異常が発生した場合でも、復旧するまで
の時間が正確に認識できるので、24時間前の周波数補正
データの利用時刻から正規の周波数補正時刻への切り換
えを正確に行うことができ、AFC機能を継続できるとい
う効果を有する。
As described above, the present invention can accurately recognize the time required for recovery even if an abnormality occurs in a received reference pilot signal by adding a timer circuit and changing the control method accompanying the timer circuit. The switching from the use time of the frequency correction data before the time to the regular frequency correction time can be accurately performed, and the AFC function can be continued.

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

第1図は本発明の一実施例のブロック図、第2図は従来
の衛星通信地球局用AFC装置のブロック図、第3図は一
般的なシステム構成図、第4図は一般的な送信周波数補
正部の構成図である。 1……タイマー回路、2……周波数カウンタ、3……CP
U、4……記憶回路、5……AFC回路、6……VCXO、7…
…分岐回路、21……地球局、22……移動体、23……衛
星、24……基準局、25……送信周波数補正部。
FIG. 1 is a block diagram of an embodiment of the present invention, FIG. 2 is a block diagram of a conventional AFC device for a satellite communication earth station, FIG. 3 is a general system configuration diagram, and FIG. FIG. 3 is a configuration diagram of a frequency correction unit. 1 ... timer circuit, 2 ... frequency counter, 3 ... CP
U, 4 ... Memory circuit, 5 ... AFC circuit, 6 ... VCXO, 7 ...
... branch circuit, 21 ... earth station, 22 ... mobile object, 23 ... satellite, 24 ... reference station, 25 ... transmission frequency correction unit.

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】衛星通信の基準局から送出される基準パイ
ロット信号を衛星を経由して受信し、前記基準パイロッ
ト信号に基づいて位相同期をかけ基準信号を作成する地
球局のAFC回路と、 前記地球局から前記衛星に向けて送信する送信信号を発
生するための電圧制御発振器と、 前記基準信号の周波数および前記送信信号の周波数を計
数する周波数カウンタと、 前記周波数カウンタに接続され、前記基準信号を基に衛
星のドプラーシフトと衛星中継器のローカル発振器の変
動を算出し、前記地球局と衛星間の周波数誤差を予め付
加するための周波数補正データとして前記電圧制御発振
器に送出する処理手段と、 前記周波数補正データを所定の時間間隔で少なくとも24
時間記憶する記憶回路と、 前記基準パイロット信号が受信されなくなってから前記
基準パイロット信号の受信が復旧されるまでの時間を計
数するタイマー回路とを備え、 前記処理手段は、 前記基準パイロット信号が受信されなかった場合に、前
記記憶回路から24時間前に記憶された周波数補正データ
を読み出し前記電圧制御発信器に供給すること、および
前記記憶回路から24時間前に記憶された周波数補正デー
タを読み出した時刻と、前記タイマー回路で計数した時
間を基に前記パイロット信号の復旧後に正規のAFC動作
を開始すべき時刻を決め、正規の周波数補正時刻に切替
える ことを特徴とする衛星通信地球局用AFC装置。
An AFC circuit of an earth station for receiving a reference pilot signal transmitted from a reference station for satellite communication via a satellite, and performing phase synchronization based on the reference pilot signal to generate a reference signal; A voltage-controlled oscillator for generating a transmission signal to be transmitted from a station toward the satellite; a frequency counter for counting the frequency of the reference signal and the frequency of the transmission signal; and Processing means for calculating the Doppler shift of the satellite and the fluctuation of the local oscillator of the satellite transponder based on the frequency control data, and transmitting the frequency error data to the voltage-controlled oscillator as frequency correction data for adding a frequency error between the earth station and the satellite in advance; At least 24 frequency correction data at predetermined time intervals
A storage circuit for storing time; and a timer circuit for counting a time from when the reference pilot signal is not received until reception of the reference pilot signal is restored, wherein the processing unit receives the reference pilot signal. If not, read the frequency correction data stored 24 hours ago from the storage circuit and supply it to the voltage control transmitter, and read the frequency correction data stored 24 hours ago from the storage circuit AFC device for a satellite communication earth station, wherein a time to start a normal AFC operation after the restoration of the pilot signal is determined based on a time and a time counted by the timer circuit, and the time is switched to a normal frequency correction time. .
JP28223690A 1990-10-19 1990-10-19 AFC device for satellite communication earth station Expired - Lifetime JP3033176B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP28223690A JP3033176B2 (en) 1990-10-19 1990-10-19 AFC device for satellite communication earth station

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP28223690A JP3033176B2 (en) 1990-10-19 1990-10-19 AFC device for satellite communication earth station

Publications (2)

Publication Number Publication Date
JPH04156728A JPH04156728A (en) 1992-05-29
JP3033176B2 true JP3033176B2 (en) 2000-04-17

Family

ID=17649831

Family Applications (1)

Application Number Title Priority Date Filing Date
JP28223690A Expired - Lifetime JP3033176B2 (en) 1990-10-19 1990-10-19 AFC device for satellite communication earth station

Country Status (1)

Country Link
JP (1) JP3033176B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5634205A (en) * 1994-04-19 1997-05-27 Uniden Corporation Radio equipment based on AFC system with temperature detection and method of automatic frequency control
ZA978516B (en) * 1996-09-30 1998-06-10 Qualcomm Inc Method and apparatus for precorrecting timing and frequency in communication systems.

Also Published As

Publication number Publication date
JPH04156728A (en) 1992-05-29

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