JPH04238419A - Pilot signal insertion circuit - Google Patents

Pilot signal insertion circuit

Info

Publication number
JPH04238419A
JPH04238419A JP629091A JP629091A JPH04238419A JP H04238419 A JPH04238419 A JP H04238419A JP 629091 A JP629091 A JP 629091A JP 629091 A JP629091 A JP 629091A JP H04238419 A JPH04238419 A JP H04238419A
Authority
JP
Japan
Prior art keywords
frequency
signal
output
mixer
reference 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.)
Pending
Application number
JP629091A
Other languages
Japanese (ja)
Inventor
Koichiro Yoshizumi
吉住 紘一郎
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 Engineering Ltd
Original Assignee
NEC Engineering Ltd
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 Engineering Ltd filed Critical NEC Engineering Ltd
Priority to JP629091A priority Critical patent/JPH04238419A/en
Publication of JPH04238419A publication Critical patent/JPH04238419A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To use a double frequency converter being a standard unit by multiplying a difference frequency between the output frequency of a crystal oscillator and a reference signal for frequency correction, and synthesizing it with an IF signal. CONSTITUTION:The multiplication degree of a phase oscillator 5 is set to be N, and the frequency of the crystal oscillator 8 to be FP/N, and the multiplication degree of an IF multiplier 10 to be N, the center value of the reference signal for frequency correction to be fR, and the frequency fluctuation of a satellite repeater to be F. Then, fR- F/N is inputted to a correction frequency inputted to a frequency correction reference signal input terminal 6 from the AFC receiver of a sea side station. Thus, fR- F/N is inputted to the output frequency of the phase synchronous oscillator 5 from the AFC receiver of the sea side station. Thus, the output frequency of the oscillator 5 becomes N(fR- F/N)=NfR- F. When the IF frequency of the communication signal in an IF input terminal is set to be fI, the output frequency of a first mixer 2 becomes fI+NfR- F, and it is corrected inversely to the frequency fluctuation of the satellite repeater. Then, frequency fluctuation is cancelled in the output of the satellite repeater.

Description

【発明の詳細な説明】[Detailed description of the invention]

【0001】0001

【産業上の利用分野】本発明は海事衛星通信地球局等に
適用されるパイロット信号挿入回路に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a pilot signal insertion circuit applied to maritime satellite communication earth stations and the like.

【0002】0002

【従来の技術】一般に海事衛星通信においては、狭帯域
のSCPC通信方式を採用しているために、衛星中継器
の局発周波数変動がチャネル間隔に比して大きく、何ら
かの方法で衛星中継器の局発周波数補正が必要となる。 特に海岸局から衛星を介して船舶局への通信においては
、船舶局側の装置を簡単にするために海岸局でその周波
数補正を行なうためパイロット信号を挿入している。
[Prior Art] In general, maritime satellite communications employ a narrowband SCPC communication system, so fluctuations in the local frequency of the satellite repeater are large compared to the channel spacing. Local frequency correction is required. Particularly in communication from a coast station to a ship station via a satellite, a pilot signal is inserted in order to correct the frequency at the coast station in order to simplify the equipment on the ship station side.

【0003】従来、この種の周波数補正用のパイロット
信号挿入回路は、図2に示すように、IF入力端子1、
第1及び第2混合器2,3、局部発振器4、位相同期発
振器5、周波数補正用基準信号入力端子6、RF出力端
子12、水晶発振器13、位相同期発振器14、合成器
15から構成される。
Conventionally, this type of pilot signal insertion circuit for frequency correction has an IF input terminal 1, as shown in FIG.
Consists of first and second mixers 2, 3, local oscillator 4, phase-locked oscillator 5, frequency correction reference signal input terminal 6, RF output terminal 12, crystal oscillator 13, phase-locked oscillator 14, and synthesizer 15 .

【0004】次にその動作を説明する。IF入力端子1
に加えられた通信用IF信号は第1混合器2で端子6に
加えられた周波数補正用基準信号に同期した位相同期発
振器5の出力と混合された後に、合成器15でパイロッ
ト信号である水晶発振器13の出力に同期した位相同期
発振器14の出力と合成され第2混合器3に入力される
。混合器3では、局部発振器4の出力と混合されRF帯
に周波数変換される。位相同期発振器14の出力はパイ
ロット信号として利用される。通信用IF信号及びパイ
ロット信号を含んだRF帯信号は海岸局から衛星へ送信
され、衛星中継器で周波数変換された後にダウン回線と
して海岸局及び船舶局へ送信される。海岸局で受信され
た衛星折り返し信号は、図示しないがAFC受信機でパ
イロット信号を利用して衛星中継器の局発周波数変動を
検出し、周波数補正基準信号を生成して周波数補正用基
準信号入力端子6へ供給する。この様にすることにより
、海岸局から送信される通信信号は衛星中継器の周波数
変動分と極性が逆の周波数補正が行われるので、衛星か
ら送信される時には衛星自体の周波数変動が相殺され、
常に一定の周波数がダウン回線に放射されることになる
。したがって船舶局では複雑なAFC装置を用いること
なく受信可能となる。
Next, its operation will be explained. IF input terminal 1
The communication IF signal applied to the terminal 6 is mixed with the output of the phase synchronized oscillator 5 synchronized with the frequency correction reference signal applied to the terminal 6 in the first mixer 2, and then mixed with the output of the phase synchronized oscillator 5 which is synchronized with the frequency correction reference signal applied to the terminal 6. It is combined with the output of the phase-locked oscillator 14 synchronized with the output of the oscillator 13 and input to the second mixer 3. The mixer 3 mixes the signal with the output of the local oscillator 4 and converts the frequency into an RF band. The output of the phase synchronized oscillator 14 is used as a pilot signal. An RF band signal including a communication IF signal and a pilot signal is transmitted from a coast station to a satellite, frequency-converted by a satellite repeater, and then transmitted as a down line to a coast station and a ship station. Although not shown, the satellite return signal received by the coast station is used by an AFC receiver to detect local frequency fluctuations of the satellite repeater using a pilot signal, generate a frequency correction reference signal, and input the reference signal for frequency correction. Supplied to terminal 6. By doing this, the communication signal transmitted from the coast station is corrected in frequency with the opposite polarity to the frequency fluctuation of the satellite repeater, so when it is transmitted from the satellite, the frequency fluctuation of the satellite itself is canceled out.
A constant frequency will always be radiated to the down line. Therefore, the ship station can receive signals without using a complicated AFC device.

【0005】[0005]

【発明が解決しようとする課題】上述した従来のパイロ
ット信号挿入回路は、パイロット信号の合成器が2重周
波数変換装置を構成する第1混合器と第2混合器との間
にあるので、第1混合器、第2混合器および局部発振器
、位相同期発振器を構成単位とする標準機器が使用出来
ないという欠点があった。
Problems to be Solved by the Invention In the conventional pilot signal insertion circuit described above, since the pilot signal combiner is located between the first mixer and the second mixer constituting the dual frequency conversion device, There was a drawback that standard equipment having the first mixer, second mixer, local oscillator, and phase-locked oscillator as constituent units could not be used.

【0006】[0006]

【課題を解決するための手段】本発明のパイロット信号
挿入回路は、衛星中継器により生ずる周波数ずれを補正
する基準信号を分配する基準信号分配器と、パイロット
信号の原振を発生する水晶発振器と、この水晶発振器の
出力信号と前記基準信号分配器の一方の出力信号とを混
合して差の周波数を出力するIF混合器と、このIF混
合器の出力をN(Nは整数)てい倍するてい倍器と、こ
のてい倍器の出力信号と通信用IF信号との和信号をと
るIF分成器と、前記基準信号分配器の他方の出力信号
に同期する位相同期発振器のNてい倍された出力信号と
前記IF合成器の出力信号とを混合する第1混合器と、
RF周波数の局部発振信号と前記第1混合器の出力信号
とを混合する第2混合器とを有する。
[Means for Solving the Problems] The pilot signal insertion circuit of the present invention includes a reference signal distributor that distributes a reference signal for correcting frequency deviation caused by a satellite repeater, and a crystal oscillator that generates the original oscillation of the pilot signal. , an IF mixer that mixes the output signal of this crystal oscillator and one output signal of the reference signal distributor and outputs a difference frequency, and the output of this IF mixer is multiplied by N (N is an integer). an IF component that takes a sum signal of the output signal of this multiplier and a communication IF signal, and a phase synchronized oscillator that is synchronized with the other output signal of the reference signal distributor. a first mixer that mixes the output signal and the output signal of the IF combiner;
It has a second mixer that mixes the local oscillation signal of the RF frequency and the output signal of the first mixer.

【0007】[0007]

【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 explained with reference to the drawings.

【0008】図1は本発明の一実施例を示すブロック図
である。図1において、図2の従来例と同一の符号は同
一の機能を有する。すなわち、本実施例では基準信号分
配器7、水晶発振器8、IF混合器9、IFてい倍器1
0、IF帯合成器11のような構成が追加されて、第1
混合器2、第2混合器3、局部発振器4、位相同期発振
器5から構成されるIF帯信号からRF帯信号へ変換す
る部分が標準機器で組み込まれている。
FIG. 1 is a block diagram showing one embodiment of the present invention. In FIG. 1, the same symbols as in the conventional example in FIG. 2 have the same functions. That is, in this embodiment, a reference signal distributor 7, a crystal oscillator 8, an IF mixer 9, an IF multiplier 1
0, a configuration such as an IF band synthesizer 11 is added, and the first
A part that converts an IF band signal into an RF band signal, which is composed of a mixer 2, a second mixer 3, a local oscillator 4, and a phase synchronized oscillator 5, is incorporated as standard equipment.

【0009】次に本実施例の動作を説明する。IF入力
端子1に加えられた通信用IF信号は、IF合成器11
で後述する水晶発振器8を原振とするパイロット信号と
合成される。合成された信号は第1混合器2で周波数補
正用基準信号入力端子6から基準信号分配器7を経由し
た基準信号に同期した位相同期発振器5の出力と混合さ
れ、和信号が生成される。この和信号はさらに第2混合
器3に入力され局部発振器4の出力と混合されて次の和
信号が生成されてRF出力端子12に供給される。一方
基準信号分配器7で分配された基準信号は、IF帯混合
器9に入力され、パイロット信号の原振である水晶発振
器8の出力と混合され、その差信号がIFてい倍器10
に入力される。IFてい倍器10の出力はパイロット信
号としてIF合成器10に加えられる。今、従来例の図
2における位相同期発振器14の出力周波数をFPとし
、図1における位相同期発振器5のてい倍次数をN、水
晶発振器8の周波数をFP/Nとし、IFてい倍器10
のてい倍次数をN、周波数補正用基準信号の中心値をf
R、衛星中継器の周波数変動分を△Fとすると、周波数
補正用基準信号入力端子6へ入力される補正周波数は従
来例と同様の手順で海岸局のAFC受信機よりfR−△
F/Nが入力される。従って位相同期発振器5の出力周
波数はN(fR−△F/N)=NfR−△Fとなる。 IF入力端子1の通信信号のIF周波数をfIとすると
、第1混合器2の出力周波数はfI+NfR−△Fとな
り、衛星中継器の周波数変動分とは逆に補正されている
ので、衛星中継器の出力では周波数変動分は打消されて
、常に一定となる。又IF帯混合器9の出力はFP/N
−(fR−△F/N)となるので、IFてい倍器10の
出力周波数はNてい倍されてN(FP/N−(fR−△
F/N))=FP−NfR+△Fとなる。IFてい倍器
10の出力はIF帯合成器11で通信信号と合成され、
第1混合器2へ入力される。次に、第1混合器2の出力
周波数は(FP−NfR+△F)+N(fR−△F/N
)=FPとなり、図2における位相同期発振器14の出
力周波数と全く同じになる。この様にパイロット信号を
IF帯で合成しても第1混合器2の出力では周波数補正
用基準信号の補正用変動分に影響されることなく、常に
一定になる。このようにIF帯でパイロットを挿入され
たIF信号を入力することにより、以降のRF信号への
変換は前述の構成の標準機器を使用することができる。
Next, the operation of this embodiment will be explained. The communication IF signal applied to the IF input terminal 1 is sent to the IF synthesizer 11.
It is combined with a pilot signal whose source oscillation is a crystal oscillator 8, which will be described later. The synthesized signal is mixed in the first mixer 2 with the output of the phase synchronized oscillator 5 synchronized with the reference signal that has passed from the frequency correction reference signal input terminal 6 through the reference signal distributor 7, and a sum signal is generated. This sum signal is further input to the second mixer 3 and mixed with the output of the local oscillator 4 to generate the next sum signal, which is supplied to the RF output terminal 12. On the other hand, the reference signal distributed by the reference signal distributor 7 is input to the IF band mixer 9, where it is mixed with the output of the crystal oscillator 8, which is the original oscillation of the pilot signal, and the difference signal is sent to the IF band mixer 10.
is input. The output of the IF multiplier 10 is applied to the IF combiner 10 as a pilot signal. Now, let FP be the output frequency of the phase-locked oscillator 14 in FIG. 2 of the conventional example, let the multiplier order of the phase-locked oscillator 5 in FIG.
The multiplication order is N, and the center value of the frequency correction reference signal is f.
R, the frequency fluctuation of the satellite repeater is △F, the correction frequency input to the frequency correction reference signal input terminal 6 is fR-△ from the AFC receiver of the coast station in the same procedure as the conventional example.
F/N is input. Therefore, the output frequency of the phase synchronized oscillator 5 is N(fR-ΔF/N)=NfR-ΔF. If the IF frequency of the communication signal at the IF input terminal 1 is fI, the output frequency of the first mixer 2 is fI + NfR - △F, which is corrected inversely to the frequency fluctuation of the satellite repeater. In the output of , the frequency fluctuation is canceled out and the output is always constant. Also, the output of the IF band mixer 9 is FP/N
-(fR-△F/N), the output frequency of the IF multiplier 10 is multiplied by N(FP/N-(fR-△F/N).
F/N))=FP-NfR+ΔF. The output of the IF multiplier 10 is combined with the communication signal by the IF band combiner 11,
It is input to the first mixer 2. Next, the output frequency of the first mixer 2 is (FP-NfR+△F)+N(fR-△F/N
)=FP, which is exactly the same as the output frequency of the phase synchronized oscillator 14 in FIG. Even if the pilot signals are combined in the IF band in this way, the output of the first mixer 2 is always constant without being affected by the correction variation of the frequency correction reference signal. By inputting the IF signal into which a pilot has been inserted in the IF band in this manner, standard equipment having the above-described configuration can be used for subsequent conversion to an RF signal.

【0010】0010

【発明の効果】以上説明したように本発明は、水晶発振
器の出力周波数と周波数補正用基準信号との差周波数を
IFてい倍器で位相同期発振器5と同じてい倍次数でて
い倍して、パイロット信号としIF帯で通信用IF信号
と合成することにより、図1に点線で示す標準機器であ
る2重周波数変換器が使用でき、生産性が向上する効果
がある。
As explained above, the present invention multiplies the difference frequency between the output frequency of the crystal oscillator and the frequency correction reference signal by the same order as that of the phase synchronized oscillator 5 using the IF multiplier. By combining the pilot signal with a communication IF signal in the IF band, it is possible to use a dual frequency converter, which is a standard device shown by a dotted line in FIG. 1, and has the effect of improving productivity.

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

【図1】本発明の一実施例のパイロット信号挿入回路の
ブロック図である。
FIG. 1 is a block diagram of a pilot signal insertion circuit according to an embodiment of the present invention.

【図2】従来のパイロット信号挿入回路のブロック図で
ある。
FIG. 2 is a block diagram of a conventional pilot signal insertion circuit.

【符号の説明】[Explanation of symbols]

1    IF入力端子 2    第1混合器 3    第2混合器 4    局部発振器 5,14    位相同期発振器 6    周波数補正用基準信号入力端子7    基
準信号分配器 8,13    水晶発振器 9    IF混合器 10    IFてい倍器 11    IF合成器 12    RF出力端子 15    合成器
1 IF input terminal 2 First mixer 3 Second mixer 4 Local oscillator 5, 14 Phase synchronized oscillator 6 Frequency correction reference signal input terminal 7 Reference signal distributor 8, 13 Crystal oscillator 9 IF mixer 10 IF multiplier 11 IF synthesizer 12 RF output terminal 15 synthesizer

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】  衛星中継器により生ずる周波数ずれを
補正する基準信号を分配する基準信号分配器と、パイロ
ット信号の原振を発生する水晶発振器と、この水晶発振
器の出力信号と前記基準信号分配器の一方の出力信号と
を混合して差の周波数を出力するIF混合器と、このI
F混合器の出力をN(Nは整数)てい倍するてい倍器と
、このてい倍器の出力信号と通信用IF信号との和信号
をとるIF分成器と、前記基準信号分配器の他方の出力
信号に同期する位相同期発振器のNてい倍された出力信
号と前記IF合成器の出力信号とを混合する第1混合器
と、RF周波数の局部発振信号と前記第1混合器の出力
信号とを混合する第2混合器とを有することを特徴とす
るパイロット信号挿入回路。
1. A reference signal distributor that distributes a reference signal for correcting frequency deviations caused by a satellite repeater, a crystal oscillator that generates an original oscillation of a pilot signal, an output signal of the crystal oscillator, and the reference signal distributor. an IF mixer that mixes the output signal of one of the two output signals and outputs the difference frequency;
A multiplier that multiplies the output of the F mixer by N (N is an integer), an IF component that takes a sum signal of the output signal of the multiplier and a communication IF signal, and the other of the reference signal distributors. a first mixer that mixes an output signal multiplied by N of a phase-locked oscillator synchronized with an output signal of the IF synthesizer, and a local oscillation signal of an RF frequency and an output signal of the first mixer. A pilot signal insertion circuit characterized by having a second mixer for mixing.
【請求項2】  前記第1混合器出力信号の周波数が周
波数補正用基準信号の補正変動分に影響されることなく
、常に一定であることを特徴とする請求項1記載のパイ
ロット信号挿入回路。
2. The pilot signal insertion circuit according to claim 1, wherein the frequency of the first mixer output signal is always constant without being affected by correction fluctuations of the frequency correction reference signal.
JP629091A 1991-01-23 1991-01-23 Pilot signal insertion circuit Pending JPH04238419A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP629091A JPH04238419A (en) 1991-01-23 1991-01-23 Pilot signal insertion circuit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP629091A JPH04238419A (en) 1991-01-23 1991-01-23 Pilot signal insertion circuit

Publications (1)

Publication Number Publication Date
JPH04238419A true JPH04238419A (en) 1992-08-26

Family

ID=11634257

Family Applications (1)

Application Number Title Priority Date Filing Date
JP629091A Pending JPH04238419A (en) 1991-01-23 1991-01-23 Pilot signal insertion circuit

Country Status (1)

Country Link
JP (1) JPH04238419A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010213352A (en) * 2010-06-14 2010-09-24 Toshiba Corp Device and method for transmitting signal

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010213352A (en) * 2010-06-14 2010-09-24 Toshiba Corp Device and method for transmitting signal

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