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JPS643099B2 - - Google Patents
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JPS643099B2 - - Google Patents

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Publication number
JPS643099B2
JPS643099B2 JP21269082A JP21269082A JPS643099B2 JP S643099 B2 JPS643099 B2 JP S643099B2 JP 21269082 A JP21269082 A JP 21269082A JP 21269082 A JP21269082 A JP 21269082A JP S643099 B2 JPS643099 B2 JP S643099B2
Authority
JP
Japan
Prior art keywords
signal
pilot signal
transmitting
pilot
phase
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
Application number
JP21269082A
Other languages
Japanese (ja)
Other versions
JPS59103433A (en
Inventor
Kenji Nagano
Toshio Nojima
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.)
NTT Inc
Original Assignee
Nippon Telegraph and Telephone 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 Nippon Telegraph and Telephone Corp filed Critical Nippon Telegraph and Telephone Corp
Priority to JP21269082A priority Critical patent/JPS59103433A/en
Publication of JPS59103433A publication Critical patent/JPS59103433A/en
Publication of JPS643099B2 publication Critical patent/JPS643099B2/ja
Granted legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/155Ground-based stations
    • H04B7/15564Relay station antennae loop interference reduction
    • H04B7/15585Relay station antennae loop interference reduction by interference cancellation

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Radio Relay Systems (AREA)

Description

【発明の詳細な説明】 本発明は送信アンテナから空間を介して受信ア
ンテナへ廻り込む干渉電波を軽減する装置に関す
るものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a device for reducing interference radio waves that go around from a transmitting antenna to a receiving antenna through space.

無線信号を受信アンテナで受信し、これを増幅
後送信アンテナより同一周波数にて再送信する無
線中継方式においては、送信アンテナから発射さ
れた信号の一部が空間を介した廻り込み電波とし
て受信アンテナに於いて再受信される場合があ
る。このような場合に、受信アンテナに於いて
は、正規の到来電波による信号と廻り込み電波に
よる干渉信号とが相加される為、中継装置の機能
を阻害する要因となり得る。従来この干渉信号を
補償する方法としては、第1図に示すように振
幅・位相を調整できる帰還回路を中継装置の送信
端から受信端の間に設け、その帰還信号を干渉信
号と逆相等振幅にすることにより干渉信号を相殺
する構成がある。図中、1は受信アンテナ、2は
送信アンテナ、3は中継増幅器、5は半固定移相
器、6は半固定減衰器、4は干渉補償のための帰
還ループである。帰還ループ4からの帰還信号が
干渉信号を相殺する条件である逆相・等振幅の条
件の設定は、半固定移相器5と半固定減衰器6の
調整により行われる。通常この調整は、測定器を
用いて手動で行われるため、極めて不便である。
また、一度調整が良好になされても、増幅器特性
や送受アンテナ間伝搬路特性の変動により干渉信
号と帰還信号との相殺状態が劣化するため、定常
的に補償特性が得られない欠点があつた。
In the wireless relay method, in which a radio signal is received by a receiving antenna, and then retransmitted at the same frequency from a transmitting antenna after being amplified, a part of the signal emitted from the transmitting antenna is transmitted to the receiving antenna as a wraparound radio wave through space. It may be re-received at some point. In such a case, at the receiving antenna, the signal due to the regular incoming radio wave and the interference signal due to the detouring radio wave are added, which may become a factor that inhibits the function of the relay device. Conventionally, as a method of compensating for this interference signal, as shown in Figure 1, a feedback circuit that can adjust the amplitude and phase is installed between the transmitting end and the receiving end of the repeater, and the feedback signal is sent to the interfering signal with the opposite phase and equal amplitude. There is a configuration that cancels the interference signal by In the figure, 1 is a receiving antenna, 2 is a transmitting antenna, 3 is a relay amplifier, 5 is a semi-fixed phase shifter, 6 is a semi-fixed attenuator, and 4 is a feedback loop for interference compensation. Setting of the conditions of opposite phase and equal amplitude, which are the conditions for the feedback signal from the feedback loop 4 to cancel the interference signal, is performed by adjusting the semi-fixed phase shifter 5 and the semi-fixed attenuator 6. This adjustment is usually done manually using a measuring instrument, which is very inconvenient.
In addition, even if the adjustment is made well, the cancellation state between the interference signal and the feedback signal deteriorates due to variations in the amplifier characteristics and the propagation path characteristics between the transmitting and receiving antennas, so there is a drawback that compensation characteristics cannot be consistently obtained. .

本発明は、これらの欠点を解決するため、受信
アンテナからパイロツト信号を送出し、そのパイ
ロツト信号について帰還ループ信号と干渉信号と
の相殺残留成分を検出することにより、帰還ルー
プ信号の振幅と位相を制御し自動的に最適補償条
件を実現し、かつ受信アンテナよりパイロツト信
号を送出することによりパイロツト信号が送信信
号に与える影響を低減するようにした干渉波補償
装置を提供するものである。
In order to solve these drawbacks, the present invention transmits a pilot signal from a receiving antenna and detects the residual component of the pilot signal that cancels out the feedback loop signal and the interference signal, thereby determining the amplitude and phase of the feedback loop signal. The present invention provides an interference wave compensator that automatically realizes optimal compensation conditions through control and transmits a pilot signal from a receiving antenna to reduce the influence of the pilot signal on a transmitted signal.

以下図面により本発明を詳細に説明する。 The present invention will be explained in detail below with reference to the drawings.

第2図は本発明の実施例であつて、1は受信ア
ンテナ、2は送信アンテナ、3は中継増幅器、4
は帰還ループ、7は等振幅2相(0゜、90゜)分配
器、8は等振幅4相(0゜、90゜、180゜、270゜)分配
器、9はパイロツト信号発生器、10はパイロツ
ト信号除去波器、11aと11bはパイロツト
信号検出波器、12と13は信号帯域通過波
器、14はレベル調整のための増幅器、15aと
15bは同期検波器、16aと16bは電圧加算
器、17は整流器、18は電気的可変減衰器、1
9a,19bは可変遅延線路である。
FIG. 2 shows an embodiment of the present invention, in which 1 is a receiving antenna, 2 is a transmitting antenna, 3 is a relay amplifier, and 4 is a transmitting antenna.
is a feedback loop, 7 is an equal amplitude 2-phase (0°, 90°) distributor, 8 is an equal amplitude 4-phase (0°, 90°, 180°, 270°) distributor, 9 is a pilot signal generator, 10 is a pilot signal remover, 11a and 11b are pilot signal detectors, 12 and 13 are signal band pass wavers, 14 is an amplifier for level adjustment, 15a and 15b are synchronous detectors, and 16a and 16b are voltage adders. 17 is a rectifier, 18 is an electrical variable attenuator, 1
9a and 19b are variable delay lines.

受信アンテナ1で受信される信号は正規の到来
電波による信号(以下正規信号という)と、送信
アンテナ2から発射後空間を介して廻り込む干渉
信号の合成されたものである。中継増幅器3の入
力信号はこれからさらに帰還ループ4を経由した
帰還信号が相加されている。さて本発明は干渉信
号と帰還信号の相殺条件を自動的に実現するもの
で、その動作は次のとおりである。いま、受信ア
ンテナ1から単一周波数のパイロツト信号が送出
されている状態を考える。このときパイロツト信
号検出波器11aの出力信号は干渉信号伝搬路
を伝搬した干渉波路信号と帰還信号との合成信号
であつて、これを第3図のベクトル図e〓sで示す。
ここで、同図中e〓i,e〓cはそれぞれ干渉波路信号お
よび帰還信号を表わす。この抽出されたパイロツ
ト信号e〓sをパイロツト信号発生器9から分岐した
信号の同相および直交成分を基準として同期検波
器15aおよび15bで同期検波すればベクトル
e〓sの同相および直交成分ex,eyが直流電圧として
検出できる。そこで、このex,eyの符号を反転し
たベクトル―e〓sをさらにe〓sに相加すればパイロツ
ト検出波器11bの出力は消失し、干渉信号と
帰還信号の相殺条件が実現できる。これは具体的
に次のようにして実現される。まず、同期検波器
15a,15bで検出された同相成分exと直交成
分eyはそれぞれ電圧加算器16aおよび16bに
入力され、その出力で等振幅4相分配器8と電気
的可変減衰器18で構成されるベクトル変調器を
駆動する。ここで、ダイオード17は電圧加算器
16a,16bの出力電圧の極性に応じてベクト
ル変調器のX軸、Y軸の極性を選択するもので、
例えばexが正ならばπ相の信号経路が導通とな
り、その導通信号のレベルは検出電圧の大きさ例
えば|es|になるように電気的可変減衰器18に
より設定される。このようにして同期検波器15
a,15bで検出された電圧に対して、ベクトル
変調器での制御を負帰還状態にすることが可能で
ある。例えば、第3図のベクトル図に示すように
送信アンテナより抽出したパイロツト信号成分の
同相成分としてex、直交成分としてeyが検出され
た場合、ベクトル変調器は帰還ループの出力信号
がそれまでの出力信号e〓cにさらに−exi−eyj(但し
i、jはそれぞれ第3図X軸、Y軸の単位ベクト
ル)すなわち−e〓sの相加された信号となる。従つ
て、この制御により送信アンテナ2により受信さ
れた信号中のパイロツト信号の抑圧が実現され
る。
The signal received by the receiving antenna 1 is a combination of a signal due to a regular arriving radio wave (hereinafter referred to as a regular signal) and an interference signal that is emitted from the transmitting antenna 2 and then circulates through space. A feedback signal via a feedback loop 4 is further added to the input signal of the relay amplifier 3. Now, the present invention automatically realizes the conditions for canceling the interference signal and the feedback signal, and its operation is as follows. Now, consider a situation where a pilot signal of a single frequency is being transmitted from the receiving antenna 1. At this time, the output signal of the pilot signal detector 11a is a composite signal of the interference wave path signal propagated through the interference signal propagation path and the feedback signal, and this is shown by the vector diagram e s in FIG.
Here, e〓 i and e〓 c in the same figure represent an interference wave path signal and a feedback signal, respectively. If this extracted pilot signal e s is synchronously detected by synchronous detectors 15a and 15b using the in-phase and quadrature components of the signal branched from the pilot signal generator 9 as references, a vector is obtained.
The in-phase and quadrature components e x and e y of e〓 s can be detected as DC voltages. Therefore, by further adding the vector −e〓 s , which is the sign-inverted vector of e . Specifically, this is achieved as follows. First, the in-phase component e x and quadrature component e y detected by the synchronous detectors 15 a and 15 b are input to voltage adders 16 a and 16 b, respectively, and the outputs thereof are used as the equal amplitude 4-phase divider 8 and the electrical variable attenuator 18. Drives a vector modulator consisting of Here, the diode 17 selects the polarity of the X-axis and Y-axis of the vector modulator according to the polarity of the output voltage of the voltage adders 16a and 16b.
For example, if e x is positive, the π-phase signal path becomes conductive, and the level of the conductive signal is set by the electrical variable attenuator 18 so that it becomes the magnitude of the detected voltage, for example, |e s |. In this way, the synchronous detector 15
It is possible to control the vector modulator in a negative feedback state with respect to the voltages detected at a and 15b. For example, as shown in the vector diagram in Figure 3, if e x is detected as the in-phase component and e y is detected as the orthogonal component of the pilot signal component extracted from the transmitting antenna, the vector modulator will detect that the output signal of the feedback loop is The output signal e〓 c is further added with −e xi −e yj (where i and j are the unit vectors of the X-axis and Y-axis in FIG. 3, respectively), that is, −e〓 s . Therefore, this control realizes suppression of the pilot signal in the signal received by the transmitting antenna 2.

さて、送信アンテナ2より送出され、受信アン
テナ1で受信される干渉信号の伝搬経路と帰還ル
ープはともに可逆性があり、前記のパイロツト信
号の抑圧条件は送信アンテナ2より送出される実
際の信号による干渉信号が帰還信号により相殺さ
れる条件に一致するので、本発明をアンテナ間干
渉の自動補償装置に応用できる。この際パイロツ
ト信号除去波器10は主信号経路のパイロツト
信号成分を除去するもので、これにより残留パイ
ロツト成分が出力側に現われることにより空間を
介して送信アンテナ2より受信されるパイロツト
信号と干渉することを防止する。なお、加算され
る制御電圧の−e〓sに対する近似性はより良い方が
収束を早めるので望ましいが、近似性が良好でな
くとも制御は負帰還となつているので収束し、干
渉信号の抑圧は可能である。また、同期検波器1
5a,15bの基準信号ならびに入力信号とベク
トル変調器の出力信号との位相同期はそれぞれ可
変遅延線路19a,19bの調整により行ない、
また、パイロツト除去波器10はパイロツト信
号が信号帯域通過波器12で十分に除去可能な
ときは不要である。
Now, the propagation path and feedback loop of the interference signal transmitted from the transmitting antenna 2 and received by the receiving antenna 1 are both reversible, and the conditions for suppressing the pilot signal described above depend on the actual signal transmitted from the transmitting antenna 2. Since this satisfies the condition that the interference signal is canceled by the feedback signal, the present invention can be applied to an automatic compensation device for inter-antenna interference. At this time, the pilot signal remover 10 removes the pilot signal component in the main signal path, so that the residual pilot component appears on the output side and interferes with the pilot signal received from the transmitting antenna 2 through space. prevent this from happening. It should be noted that it is desirable that the approximation of the added control voltage to −e〓 s is better because convergence will be faster, but even if the approximation is not good, since the control is negative feedback, it will converge and the interference signal will be suppressed. is possible. In addition, the synchronous detector 1
The phase synchronization between the reference signals and input signals of the vector modulators 5a and 15b and the output signal of the vector modulator is performed by adjusting the variable delay lines 19a and 19b, respectively.
Further, the pilot remover 10 is not necessary when the pilot signal can be sufficiently removed by the signal bandpass remover 12.

以上説明したように、本発明を用いることによ
り、アンテナ受信信号において干渉波信号をアン
テナ送受間伝搬路および中継増幅器の特性変動と
無関係に自動的に低減することが可能となるか
ら、送受信号周波数が同一である無線中継方式に
おいて送受アンテナ間の干渉信号を補償すること
ができ、中継装置の増幅利得として送受アンテナ
間結合減衰量(干渉補償を用いない場合の値)以
上のものを配分できる。また、受信アンテナより
パイロツト信号を送出することから、送信信号に
混入するパイロツト信号のレベルは極めて低くな
るため、パイロツト信号を挿入したことにより中
継増幅する信号にパイロツト信号による干渉歪が
発生するといつた悪影響が生ずることを防止でき
る利点がある。
As explained above, by using the present invention, it is possible to automatically reduce the interference wave signal in the antenna reception signal regardless of the characteristic fluctuations of the propagation path between the antenna transmission and reception and the relay amplifier. It is possible to compensate for interference signals between transmitting and receiving antennas in a wireless relay system in which the transmitting and receiving antennas are the same, and it is possible to allocate more than the coupling attenuation between the transmitting and receiving antennas (the value when no interference compensation is used) as the amplification gain of the relay device. In addition, since the pilot signal is sent from the receiving antenna, the level of the pilot signal mixed in with the transmitted signal is extremely low, so inserting the pilot signal may cause interference distortion in the signal to be relayed and amplified. This has the advantage of preventing adverse effects from occurring.

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

第1図は従来の干渉補償装置の一例を示すブロ
ツク図、第2図は本発明の一実施例を示すブロツ
ク図、第3図は受信パイロツト信号のベクトル図
である。 1…受信アンテナ、2…送信アンテナ、3…中
継増幅器、4…帰還ループ、5…半固定移相器、
6…半固定減衰器、7…等振幅2相分配器、8…
等振幅4相分配器、9…パイロツト信号発生器、
10…パイロツト信号除去波器、11…パイロ
ツト信号検出波器、12,13…信号帯域通過
波器、14…増幅器、15a,15b…同期検
波器、16a,16b…電圧加算器、17…ダイ
オード、18…電気的可変減衰器、19a,19
b…可変遅延線路、20…抽出されたパイロツト
信号ベクトル、21…干渉信号ベクトル、22…
帰還信号ベクトル、23…パイロツト信号の逆ベ
クトル、24…パイロツト信号ベクトルのX成分
(同相成分)、25…パイロツト信号ベクトルのY
成分(直交成分)、26a,26b…サーキユレ
ータ。
FIG. 1 is a block diagram showing an example of a conventional interference compensation device, FIG. 2 is a block diagram showing an embodiment of the present invention, and FIG. 3 is a vector diagram of a received pilot signal. 1... Receiving antenna, 2... Transmitting antenna, 3... Relay amplifier, 4... Feedback loop, 5... Semi-fixed phase shifter,
6... Semi-fixed attenuator, 7... Equal amplitude two-phase distributor, 8...
Equal amplitude 4-phase distributor, 9...pilot signal generator,
10... Pilot signal remover, 11... Pilot signal detector, 12, 13... Signal bandpass waver, 14... Amplifier, 15a, 15b... Synchronous detector, 16a, 16b... Voltage adder, 17... Diode, 18...Electrical variable attenuator, 19a, 19
b...Variable delay line, 20...Extracted pilot signal vector, 21...Interference signal vector, 22...
Feedback signal vector, 23... Inverse vector of the pilot signal, 24... X component (in-phase component) of the pilot signal vector, 25... Y of the pilot signal vector
Components (orthogonal components), 26a, 26b...circulator.

Claims (1)

【特許請求の範囲】[Claims] 1 無線信号を受信アンテナで受信した受信信号
を増幅器で増幅し該受信信号と同一周波数で送信
アンテナから送信信号として再送信する無線中継
装置において、前記受信アンテナより特定周波数
のパイロツト信号を送出する手段と、前記送信ア
ンテナより該パイロツト信号を抽出する手段と、
前記受信信号へ廻り込む前記パイロツト信号を除
去して前記受信信号を前記増幅器に印加する手段
と、前記パイロツト信号及び前記送信信号の一部
を分岐して振幅・位相を調整するためのベクトル
変調器に印加する手段と、該ベクトル変調器の送
信信号出力とパイロツト信号出力とを前記受信信
号の経路及び前記送信信号の経路にそれぞれ帰還
する手段と、前記送信アンテナから抽出したパイ
ロツト信号の同相成分および直交成分を検出する
手段と、検出された同相成分および直交成分の情
報により前記ベクトル変調器を制御する手段とを
有し、前記送信アンテナより空間を介して前記受
信アンテナに帰還する干渉信号を低減させるよう
に構成されたことを特徴とする干渉波補償装置。
1. In a radio relay device that receives a radio signal with a receiving antenna, amplifies the received signal with an amplifier, and retransmits it as a transmitting signal from the transmitting antenna at the same frequency as the received signal, means for transmitting a pilot signal of a specific frequency from the receiving antenna. and means for extracting the pilot signal from the transmitting antenna;
means for removing the pilot signal that goes around to the received signal and applying the received signal to the amplifier; and a vector modulator for branching part of the pilot signal and the transmitted signal to adjust amplitude and phase. means for feeding back the transmitted signal output and the pilot signal output of the vector modulator to the received signal path and the transmitted signal path, respectively; It has means for detecting orthogonal components, and means for controlling the vector modulator based on information on the detected in-phase and orthogonal components, and reduces interference signals that return from the transmitting antenna to the receiving antenna through space. An interference wave compensator characterized in that it is configured to.
JP21269082A 1982-12-06 1982-12-06 Compensating device of interference wave Granted JPS59103433A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21269082A JPS59103433A (en) 1982-12-06 1982-12-06 Compensating device of interference wave

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21269082A JPS59103433A (en) 1982-12-06 1982-12-06 Compensating device of interference wave

Publications (2)

Publication Number Publication Date
JPS59103433A JPS59103433A (en) 1984-06-14
JPS643099B2 true JPS643099B2 (en) 1989-01-19

Family

ID=16626807

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21269082A Granted JPS59103433A (en) 1982-12-06 1982-12-06 Compensating device of interference wave

Country Status (1)

Country Link
JP (1) JPS59103433A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08251094A (en) * 1995-03-15 1996-09-27 Hitachi Ltd Satellite communication system and method
IL137078A (en) * 1999-07-20 2005-05-17 Andrew Corp Side-to-side repeater and adaptive cancellation for repeater
US6385435B1 (en) * 2000-04-20 2002-05-07 Jhong Sam Lee Coupled interference concellation system for wideband repeaters in a cellular system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55133148A (en) * 1979-04-04 1980-10-16 Nippon Telegr & Teleph Corp <Ntt> Interference wave removal system
GB2052216B (en) * 1979-06-08 1983-09-21 Plessey Co Ltd Duplex transceivers

Also Published As

Publication number Publication date
JPS59103433A (en) 1984-06-14

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