JPS61214806A - Am detecting circuit - Google Patents

Am detecting circuit

Info

Publication number
JPS61214806A
JPS61214806A JP5666985A JP5666985A JPS61214806A JP S61214806 A JPS61214806 A JP S61214806A JP 5666985 A JP5666985 A JP 5666985A JP 5666985 A JP5666985 A JP 5666985A JP S61214806 A JPS61214806 A JP S61214806A
Authority
JP
Japan
Prior art keywords
signal
circuit
pilot signal
amplitude
input terminal
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
JP5666985A
Other languages
Japanese (ja)
Inventor
Katsuhiko Honda
本多 克彦
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.)
Fujitsu General Ltd
Original Assignee
Fujitsu General 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 Fujitsu General Ltd filed Critical Fujitsu General Ltd
Priority to JP5666985A priority Critical patent/JPS61214806A/en
Publication of JPS61214806A publication Critical patent/JPS61214806A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To suppress the variation of amplitude and to improve the articulation of a detected and demodulated sound signal by inserting a PLL circuit between a pilot signal extracting circuit and a homodyne detecting circuit. CONSTITUTION:A pilot signal extracted from an SSB signal by a pilot signal extracting circuit 14 is amplified by an amplifier circuit 20 of a PLL circuit 19 and is given to a phase comparing circuit 22 as a reference frequency input signal. A signal from a VCO 21 whose frequency is approximately equal to that of the pilot signal is inputted to the comparing circuit 22. When phases of both signals are synchronized with each other, the signal from the VCO 21 is equal to the pilot signal and has a certain amplitude. This phase synchronized signal is inputted to the other input terminal 15b of a homodyne detecting circuit 10. As the result, the output is held down by K-number of times when the whole of the signal is increased by K-number of times because of the variance of amplitude. Thus, the articulation of the detected and demodulated sound signal is improved considerably.

Description

【発明の詳細な説明】 「産業上の利用分野」 本発明はパイロット用搬送波信号を伴った単側帯波(S
 S B)信号から変調信号を復調するホモダイン検波
において、伝搬路でのフェーディング等により入力信号
に振幅変動があっても検波出力の変化を可能な限り少な
くして音声の明瞭度の改善を図ったAM検波回路に関す
るものである。
DETAILED DESCRIPTION OF THE INVENTION "Industrial Application Field" The present invention is directed to a single sideband (S)
S B) In homodyne detection, which demodulates the modulated signal from the signal, even if there is amplitude fluctuation in the input signal due to fading in the propagation path, the change in the detection output is minimized to improve speech clarity. The present invention relates to an AM detection circuit.

「従来の技術」 パイロット用搬送波信号を伴ったSSB信号とは基本的
には特公昭33−9159号公報に示されているいわゆ
るリンコンベックス方式の信号を指すものとする。この
リンコンベックス方式は、音声信号の振幅と周波数の成
分をそれぞれ分離して振幅成分は周波数変調(FM)さ
れた周波数情報に変換し、また周波数成分は一定振幅化
して伝送し、受信側ではFM周波数情報に基づいて元の
振幅成分に戻して音声信号を得る方式である。
"Prior Art" The SSB signal accompanied by a pilot carrier signal basically refers to a so-called Rinconvex signal as disclosed in Japanese Patent Publication No. 33-9159. This Rinconvex method separates the amplitude and frequency components of an audio signal, converts the amplitude component into frequency modulated (FM) frequency information, and transmits the frequency component as a constant amplitude. This is a method to obtain an audio signal by restoring the original amplitude component based on frequency information.

この方式を移動通信に用いる場合、伝搬路におけるレー
レ−フェーディングによる電界変動のため、受信機に到
来する電波が激しく変化する。一定振幅化された周波数
成分がフ二一ディングにより変化してしまうとFM情報
のみならずフエーディングで音声信号の大きさが変って
しまう。また、FM情報を振幅情報に正しく戻すために
も振幅が安定していることが望ましい。そのため従来は
When this system is used for mobile communications, the radio waves arriving at the receiver change drastically due to electric field fluctuations due to Rayleigh fading in the propagation path. If the frequency component, which has a constant amplitude, changes due to fading, not only the FM information but also the magnitude of the audio signal will change due to fading. Furthermore, it is desirable that the amplitude be stable in order to correctly return FM information to amplitude information. Therefore, conventionally.

応答の速い自動利得制御(AGC)回路で振幅変動を抑
えるようにしていた。従来の具体的回路が第2図に示さ
れる。この第2図において、アンテナ(1)に到来した
例えばVHF帯のSSB信号は、受信部(2)の高周波
増幅回路(3)で増幅され、混合回路(4)で中間周波
数に変換されて中間周波増幅回路(5)・・・(6)で
増幅される。この出力は、通、常はAGC回路(7)を
介して前記増幅回路(3) (5)・・・(6)に帰還
され一定利得に制御される。この利得制御された信号は
ホモダイン検波部(8)の増幅回路(9)で増幅されホ
モダイン検波回路(10)の一方の入力端子(15a)
にそのまま入力するとともに、増幅回路(11)、パイ
ロット信号抽出用フィルタ回路(12)。
Amplitude fluctuations were suppressed using a fast-response automatic gain control (AGC) circuit. A specific conventional circuit is shown in FIG. In Fig. 2, an SSB signal in the VHF band, for example, which has arrived at the antenna (1) is amplified by the high frequency amplification circuit (3) of the receiving section (2), converted to an intermediate frequency by the mixing circuit (4), and then It is amplified by frequency amplification circuits (5)...(6). This output is normally fed back to the amplifier circuits (3), (5), . . . (6) via the AGC circuit (7) and is controlled to a constant gain. This gain-controlled signal is amplified by the amplifier circuit (9) of the homodyne detection section (8) and sent to one input terminal (15a) of the homodyne detection circuit (10).
input as is, an amplifier circuit (11), and a pilot signal extraction filter circuit (12).

増幅回路(13)からなるパイロット信号抽出回路(1
4)を経て抽出されたパイロット信号が前記ホモダイン
検波回路(10)の他方の入力端子(isb)に入力す
る。このホモダイン検波回路(10)ではつどのような
2つの入力信号の積に比例した出力が得られる。
A pilot signal extraction circuit (1) consisting of an amplifier circuit (13)
The pilot signal extracted through step 4) is input to the other input terminal (isb) of the homodyne detection circuit (10). This homodyne detection circuit (10) provides an output proportional to the product of two input signals.

ここで、到来信号成分はパイロット搬送波信号foと、
音声で変調されたSSB被変調波信号faからなり、ホ
モダイン検波回路(10)の一方の入力端子(15b)
に加わる信号を、A 1 cosfo + B cos
faとし、他方の入力端子(15b)に加わる信号をA
 2 CogfOとすると、 出力ac (A 1 cosfo + B cosfa
) A 2 cosf。
Here, the arriving signal component is a pilot carrier signal fo,
Consisting of the SSB modulated wave signal fa modulated by audio, one input terminal (15b) of the homodyne detection circuit (10)
The signal applied to A 1 cosfo + B cos
fa, and the signal applied to the other input terminal (15b) is A.
2 CogfO, output ac (A 1 cosfo + B cosfa
) A2cosf.

cos(fa−fo)) となり、これがホモダイン検波回路(10)から出力す
る。この式において、第1項の直流分、第2項、第3項
をそれぞれ直流カット用コンデンサおよびLPF(ロー
パスフィルタ回路) (16)で除くと、最終的な出力
として 2B −cos(fa fo)の成分が得られる。
cos(fa-fo)), which is output from the homodyne detection circuit (10). In this equation, if the DC component of the first term, the second term, and the third term are respectively removed by a DC cut capacitor and an LPF (low-pass filter circuit) (16), the final output is 2B - cos (fa fo) The following components are obtained.

この成分中のfa −foは元の音声変調信号であるか
ら、これを低周波増幅回路(17)で増幅し、スピーカ
(18)で音声を聞くことができる。
Since fa-fo in this component is the original audio modulation signal, it can be amplified by the low frequency amplifier circuit (17) and the audio can be heard through the speaker (18).

「発明が解決しようとする問題点」 今、伝搬路によるフェーディングによって振幅変動を受
けた場合、AGC回路(7)はこの変動分を補償するよ
うに動作する。しかし、AGC回路(7)の動作の遅延
や動作レベル範囲等により、振幅変動を完全に抑え切れ
ず、振幅変動が残った状態でホモダイン検波部(8)へ
入力される。この場合、振幅変動により前記信号 2B −−cos(fa−fo)かに倍されると、出力におい
て、となって、K2倍に出力変動が増大してしまう。
"Problems to be Solved by the Invention" Now, when amplitude fluctuation is caused by fading due to the propagation path, the AGC circuit (7) operates to compensate for this fluctuation. However, due to operational delays and operating level ranges of the AGC circuit (7), amplitude fluctuations cannot be completely suppressed, and the remaining amplitude fluctuations are input to the homodyne detection section (8). In this case, if the signal 2B --cos(fa-fo) is multiplied by the amplitude fluctuation, the output fluctuation will increase by a factor of K2.

このため、音声が不自然な大きさに変化して聞きづらく
、明瞭度を悪くするという欠点があった。
As a result, the sound changes to an unnatural volume, making it difficult to hear and reducing clarity.

「問題点を解決するための手段」 本発明は上述のような問題点を解決するためにされたも
ので、ホモダイン検波回路の一方の入力端子に、パイロ
ット信号を伴ったAM信号を加え。
``Means for Solving the Problems'' The present invention was made to solve the above-mentioned problems, and involves adding an AM signal accompanied by a pilot signal to one input terminal of a homodyne detection circuit.

前記ホモダイン検波回路の他方の入力端子に、パイロッ
ト信号抽出回路で抽出したパイロット信号を加え、これ
らの信号から変調信号を復調するようにしたAM検波回
路において、前記パイロット信号抽出回路と、前記ホモ
ダイン検波回路の他方の入力端子との間に、リファレン
ス信号として入力した前記パイロット信号と電圧制御発
振回路からの信号とを位相比較器で位相比較し、位相同
期が得られたときの前記電圧制御発振回路の出力を前記
ホモダイン検波回路へ入力するためのPLL回路を挿入
してなるものである。
A pilot signal extracted by a pilot signal extraction circuit is added to the other input terminal of the homodyne detection circuit, and a modulated signal is demodulated from these signals. A phase comparator compares the phases of the pilot signal inputted as a reference signal with the signal from the voltage controlled oscillation circuit between the other input terminal of the circuit, and the voltage controlled oscillation circuit when phase synchronization is obtained. A PLL circuit is inserted for inputting the output of the circuit to the homodyne detection circuit.

「作用」 到来したSSB信号を受信部で中間周波信号に変換する
。この中間周波信号は一方ではそのままホモダイン検波
回路の一方の入力端子に加える。
"Operation" The incoming SSB signal is converted into an intermediate frequency signal at the receiving section. On the one hand, this intermediate frequency signal is applied as is to one input terminal of the homodyne detection circuit.

他方では中間周波信号からパイロット信号抽出回路で抽
出されたパイロット信号を、リファレンス信号としてP
LL回路に加え、このPLL回路の電圧制御発振回路(
VCO)からの信号と位相比較器で位相比較し、位相同
期が得られたときのvC0の出力をホモダイン検波回、
路の他方の入力端子に加える。これらの入力信号から変
調信号を復調する。すると、振幅変動で信号全体かに倍
となっても出力もに倍に抑えられ音声の明瞭度が改善さ
れる。
On the other hand, the pilot signal extracted from the intermediate frequency signal by the pilot signal extraction circuit is used as the reference signal P
In addition to the LL circuit, this PLL circuit's voltage controlled oscillation circuit (
The phase of the signal from VCO) is compared with the phase comparator, and when phase synchronization is obtained, the output of vC0 is sent to the homodyne detection circuit,
to the other input terminal of the circuit. A modulated signal is demodulated from these input signals. Then, even if the overall signal doubles due to amplitude fluctuations, the output is suppressed to double, improving the clarity of the voice.

「実施例」 以下、本発明の一実施例を第1図に基づいて説明する。"Example" Hereinafter, one embodiment of the present invention will be described based on FIG.

第1図の本発明の回路と第2図の従来の回路との異なる
点は、中間周波信号からパイロット信号を抽出するため
のパイロット信号抽出回路(14)と、ホモダイン検波
回路(10)の他方の入力端子(15b)との間に、p
 L L (Phase Locked Loop)回
路(19)を挿入したことである。このPLL回路(1
9)は、パイロット信号を増幅する増幅回路(20)、
抽出されたパイロット信号と電圧制御発振回路(VCO
)(21)の信号と位相比較する位相比較回路(22)
およびローパスフィルタ回路(L P F)(23)で
構成され、前記V CO(21)の出力側が前記ホモダ
イン検波回路(10)の他方の入力端子(15b)に結
合されている。
The difference between the circuit of the present invention shown in FIG. 1 and the conventional circuit shown in FIG. between the input terminal (15b) of p
This is because an LL (Phase Locked Loop) circuit (19) is inserted. This PLL circuit (1
9) is an amplification circuit (20) that amplifies the pilot signal;
Extracted pilot signal and voltage controlled oscillator circuit (VCO)
) (21) Phase comparison circuit (22) that compares the phase with the signal of (21)
and a low-pass filter circuit (LPF) (23), and the output side of the VCO (21) is coupled to the other input terminal (15b) of the homodyne detection circuit (10).

その他の部分は第2図と同一であるから同一符号を付す
Other parts are the same as those in FIG. 2, so the same reference numerals are given.

以上のような構成において、PLL回路(19)に入力
するまでの動作は第2図の従来の回路と変わるところは
ない。
In the above configuration, the operation up to input to the PLL circuit (19) is the same as that of the conventional circuit shown in FIG.

パイロット信号抽出回路(14)でSSB信号から抽出
されたパイロット信号は、PLL回路(19)の増幅回
路(20)で増幅され、この信号がリファレンス周波入
力信号として位相比較回路(22)に入力される。この
位相比較回路(22)にはまたV CO(21)からパ
イロット信号と略等しい周波数の信号が入力している。
The pilot signal extracted from the SSB signal by the pilot signal extraction circuit (14) is amplified by the amplifier circuit (20) of the PLL circuit (19), and this signal is input to the phase comparison circuit (22) as a reference frequency input signal. Ru. A signal having substantially the same frequency as the pilot signal is also input to the phase comparator circuit (22) from the VCO (21).

そして両者の信号の位相同期が得られたとき、V CO
(21)からの信号がパイロット信号に等しく、また一
定振幅となる。この位相同期した信号がホモダイン検波
回路(10)の他方の入力端子(15b)に入力する。
When the phase synchronization of both signals is obtained, V CO
The signal from (21) is equal to the pilot signal and has a constant amplitude. This phase-synchronized signal is input to the other input terminal (15b) of the homodyne detection circuit (10).

この結果、振幅変動により信号全体かに倍となったとき
、出力は。
As a result, when the entire signal doubles due to amplitude variation, the output is.

となり、出力もに倍に抑えられる。Therefore, the output can be doubled.

「発明の効果」 本発明は上述のように、信号波から抽出したパイロット
信号をリファレンス周波入力としてvCOの発振信号を
これに位相同期させ、このときのvCOの出力をホモダ
イン検波回路の他方の入力端子に加えたので、伝搬路で
のフ二一ディング等により入力信号の振幅変動かに倍に
なっても出力変動もに倍で抑えられ、検波・復調された
音声信号の明瞭度が大巾に改善される。
"Effects of the Invention" As described above, the present invention uses a pilot signal extracted from a signal wave as a reference frequency input, synchronizes the phase of the oscillation signal of the vCO with this, and outputs the output of the vCO at this time as the other input of the homodyne detection circuit. Since it is applied to the terminal, even if the amplitude fluctuation of the input signal doubles due to fusing in the propagation path, the output fluctuation is suppressed to twice as much, and the clarity of the detected and demodulated audio signal is greatly improved. will be improved.

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

第1図は本発明によるAM検波回路の一実施例を示すブ
ロック図、第2図は従来の回路のブロック図である。 (1)・・・アンテナ、(2)・・・受信部、(3)・
・・高周波増幅回路、(4)・・・混合回路、(5) 
(6)・・・中間周波増幅回路、(7)・・・AGC回
路、(8)・・・ホモダイン検波部。 (9) (11) (13) (20)・・・増幅回路
、(10)・・・ホモダイン検波回路、(12)・・・
フィルタ回路、(14)・・・パイロット信号抽出回路
、(15a)・・・一方の入力端子、(15b)・・・
他方の入力端子、(16) (23)・・・LPF、(
17)・・・低周波増幅回路、 (18)・・・スピー
カ、(19)・・・PLL回路、 (21)・・・VC
Ol(22)・・・位相比較回路。
FIG. 1 is a block diagram showing an embodiment of an AM detection circuit according to the present invention, and FIG. 2 is a block diagram of a conventional circuit. (1)... Antenna, (2)... Receiving section, (3)...
...High frequency amplifier circuit, (4)...Mixing circuit, (5)
(6)...Intermediate frequency amplifier circuit, (7)...AGC circuit, (8)...Homodyne detection section. (9) (11) (13) (20)... Amplifier circuit, (10)... Homodyne detection circuit, (12)...
Filter circuit, (14)...Pilot signal extraction circuit, (15a)...One input terminal, (15b)...
The other input terminal, (16) (23)...LPF, (
17)...Low frequency amplifier circuit, (18)...Speaker, (19)...PLL circuit, (21)...VC
Ol(22)...Phase comparison circuit.

Claims (1)

【特許請求の範囲】[Claims] (1)ホモダイン検波回路の一方の入力端子に、パイロ
ット信号を伴ったAM信号を加え、前記ホモダイン検波
回路の他方の入力端子に、パイロット信号抽出回路で抽
出したパイロット信号を加え、これらの信号から変調信
号を復調するようにしたAM検波回路において、前記パ
イロット信号抽出回路と、前記ホモダイン検波回路の他
方の入力端子との間に、リファレンス信号として入力し
た前記パイロット信号と電圧制御発振回路からの信号と
を位相比較器で位相比較し、位相同期が得られたときの
前記電圧制御発振回路の出力を前記ホモダイン検波回路
へ入力するためのPLL回路を挿入してなることを特徴
とするAM検波回路。
(1) Add an AM signal with a pilot signal to one input terminal of the homodyne detection circuit, add the pilot signal extracted by the pilot signal extraction circuit to the other input terminal of the homodyne detection circuit, and extract from these signals. In an AM detection circuit configured to demodulate a modulated signal, the pilot signal input as a reference signal and a signal from the voltage controlled oscillation circuit are provided between the pilot signal extraction circuit and the other input terminal of the homodyne detection circuit. and a PLL circuit for inputting the output of the voltage controlled oscillation circuit to the homodyne detection circuit when phase synchronization is obtained. .
JP5666985A 1985-03-20 1985-03-20 Am detecting circuit Pending JPS61214806A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5666985A JPS61214806A (en) 1985-03-20 1985-03-20 Am detecting circuit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5666985A JPS61214806A (en) 1985-03-20 1985-03-20 Am detecting circuit

Publications (1)

Publication Number Publication Date
JPS61214806A true JPS61214806A (en) 1986-09-24

Family

ID=13033823

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5666985A Pending JPS61214806A (en) 1985-03-20 1985-03-20 Am detecting circuit

Country Status (1)

Country Link
JP (1) JPS61214806A (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5366110A (en) * 1976-11-26 1978-06-13 Hitachi Ltd Waveform transmitting system

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5366110A (en) * 1976-11-26 1978-06-13 Hitachi Ltd Waveform transmitting system

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