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JP2010066069A - Secondary surveillance radar system - Google Patents

Secondary surveillance radar system Download PDF

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JP2010066069A
JP2010066069A JP2008231173A JP2008231173A JP2010066069A JP 2010066069 A JP2010066069 A JP 2010066069A JP 2008231173 A JP2008231173 A JP 2008231173A JP 2008231173 A JP2008231173 A JP 2008231173A JP 2010066069 A JP2010066069 A JP 2010066069A
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signal
difference
amplitude
processing unit
compensation amount
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JP2010066069A5 (en
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Toshio Nanba
敏男 難波
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Toshiba Corp
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Abstract

【課題】給電系が変化した場合において、各チャンネル間の振幅・位相特性の調整を自動で行うことが可能となり、これにより運用における長期間の安定度の確保が可能な二次監視レーダ装置を提供する。
【解決手段】空中線装置3で得られる和パターンΣ及び差パターンΔに代えて、オムニパターンの給電系上のパイロット信号発生回路7で生成される既知の振幅・位相特性を有するパイロット信号をパイロット注入回路8にて和パターンΣのチャンネル及び差パターンΔのチャンネルに注入し、これらチャンネルの試験信号を利用して、振幅/位相検出回路12にて各チャンネル間の信号の振幅差及び位相差を検出し、比較回路14にて予め保持部13に保持されている基準値と比較することで、設置条件の変更等により給電系が変化したか否かを判断し、変化した場合には、変化したことによるチャンネル間の信号の振幅・位相特性を自動で調整するようにしている。
【選択図】 図2
[PROBLEMS] To provide a secondary monitoring radar device capable of automatically adjusting amplitude and phase characteristics between channels when a feeding system is changed, thereby ensuring long-term stability in operation. provide.
A pilot signal having a known amplitude / phase characteristic generated by a pilot signal generation circuit on an omni-pattern feeding system is pilot-injected in place of a sum pattern Σ and a difference pattern Δ obtained by an antenna apparatus. The circuit 8 injects into the channel of the sum pattern Σ and the channel of the difference pattern Δ, and the amplitude / phase detection circuit 12 detects the amplitude difference and phase difference between the channels by using the test signals of these channels. Then, by comparing with the reference value held in the holding unit 13 in advance by the comparison circuit 14, it is determined whether or not the power feeding system has changed due to a change in installation conditions or the like. The amplitude / phase characteristics of signals between channels are automatically adjusted.
[Selection] Figure 2

Description

この発明は、例えば航空管制用の二次監視レーダ装置に関する。   The present invention relates to a secondary monitoring radar device for air traffic control, for example.

航空管制用の二次監視レーダ装置は、例えば非特許文献1に示されているように、質問信号をターゲットとなる航空機上のトランスポンダ(応答装置)に送信し、このトランスポンダからの質問信号に対応する応答信号を受信することによって航空機の識別を行なうものである。この場合、モノパルス測角方式により航空機の距離及び方位を求めている。
二次レーダ理論。
As shown in Non-Patent Document 1, for example, the secondary surveillance radar device for air traffic control transmits a question signal to a transponder (response device) on a target aircraft and responds to the question signal from the transponder. The aircraft is identified by receiving a response signal. In this case, the distance and direction of the aircraft are obtained by the monopulse angle measurement method.
Secondary radar theory.

ところで、上記二次監視レーダ装置では、モノパルス測角方式で使用するマルチ受信機を備える場合に、測角精度を向上させるために、各チャンネル間(和パターン、差パターン)の振幅・位相特性を同一にする必要がある。この場合、各チャンネル間の振幅・位相特性を測定し、この測定結果に基づいて、振幅/位相調整回路の調整を人為的作業によって行なっている。このため、調整が完了するまでに多くの手間と時間がかかり、また調整精度の確保が難しく、運用における長期間の安定度の確保が難しい。   By the way, when the secondary monitoring radar apparatus includes a multi-receiver used in the monopulse angle measurement method, the amplitude / phase characteristics between the channels (sum pattern, difference pattern) are improved in order to improve angle measurement accuracy. Must be the same. In this case, the amplitude / phase characteristics between the channels are measured, and the amplitude / phase adjustment circuit is adjusted by human work based on the measurement result. For this reason, it takes a lot of labor and time to complete the adjustment, it is difficult to ensure the adjustment accuracy, and it is difficult to ensure the long-term stability in operation.

また、設置条件の変更等により給電系が変化した場合には、振幅/位相調整回路における再調整が必要となる。   Further, when the power feeding system changes due to a change in installation conditions or the like, readjustment in the amplitude / phase adjustment circuit is necessary.

そこで、この発明の目的は、給電系が変化した場合において、各チャンネル間の振幅・位相特性の調整を自動で行うことが可能となり、これにより運用における長期間の安定度の確保が可能な二次監視レーダ装置を提供することにある。   Accordingly, an object of the present invention is to automatically adjust the amplitude and phase characteristics between the channels when the power feeding system changes, thereby ensuring long-term stability in operation. It is to provide a next monitoring radar device.

上記目的を達成するために、この発明に係る二次監視レーダ装置は、目標対象物からの第1の信号を空中線装置にて受信し、空中線装置の複数エレメントで得られる各受信信号の和信号を第1系統へ、各受信信号の差信号を第2系統へ分岐して目標処理部に入力すると共に、目標対象物と目標処理部との間で第1の信号に対する誤応答を防止するための第2の信号を第3系統を介して送受信し、目標処理部にて和信号、差信号及び第2の信号から目標対象物に関する目標情報を得る二次監視レーダ装置において、第3系統に設けられ、和信号及び差信号に対しそれぞれ既知の振幅・位相特性を有する試験信号を発生する試験信号発生手段と、試験信号送出時に、和信号及び差信号に代わって試験信号を第1及び第2系統に注入する試験信号注入手段と、試験信号送出時に、第1及び第2系統間の試験信号の振幅差及び位相差を検出する検出手段と、この検出手段による検出結果から補償量を求める補償量演算手段と、この補償量演算手段で得られた補償量に基づいて、第1及び第2系統間の試験信号の振幅・位相特性を補償して目標処理部に出力する補償手段とを備えるようにしたものである。   In order to achieve the above object, a secondary monitoring radar apparatus according to the present invention receives a first signal from a target object by an antenna apparatus, and a sum signal of received signals obtained by a plurality of elements of the antenna apparatus. To the first system, the difference signal of each received signal is branched to the second system and input to the target processing unit, and an erroneous response to the first signal is prevented between the target object and the target processing unit. In the secondary monitoring radar apparatus that transmits / receives the second signal of the second target signal via the third system and obtains target information regarding the target object from the sum signal, the difference signal, and the second signal in the target processing unit, Provided is a test signal generating means for generating a test signal having known amplitude and phase characteristics with respect to the sum signal and the difference signal, and the first and first test signals instead of the sum signal and the difference signal when the test signal is transmitted. Test signal injected into two systems Note Means, detecting means for detecting the amplitude difference and phase difference of the test signal between the first and second systems when the test signal is transmitted, a compensation amount calculating means for obtaining a compensation amount from the detection result by the detecting means, and the compensation Compensation means for compensating the amplitude / phase characteristics of the test signal between the first and second systems based on the compensation amount obtained by the quantity calculation means and outputting the compensation signal to the target processing unit is provided.

なお、補償量演算手段は、予め和信号と差信号との振幅差及び位相差が一意に定まる基準値を保持する基準値保持手段と、検出手段で検出される振幅差及び位相差と基準値保持手段で保持されている基準値とを比較することで、補償量を求める比較手段とを備える。   The compensation amount calculating means includes a reference value holding means for holding a reference value for uniquely determining an amplitude difference and a phase difference between the sum signal and the difference signal, and an amplitude difference, a phase difference and a reference value detected by the detecting means. Comparing means for obtaining a compensation amount by comparing with a reference value held by the holding means.

この構成によれば、和信号及び差信号に代えて、第3系統から送られ既知の振幅・位相特性を有する試験信号を第1系統及び第2系統に注入し、これら第1系統及び第2系統の試験信号を利用して、各系統間の信号の振幅差及び位相差を検出して予め保持されている基準値と比較することで、設置条件の変更等により給電系が変化したか否かを判断し、変化した場合には、変化したことによる系統間の試験信号の振幅及び位相特性を自動で補償するようにしている。   According to this configuration, instead of the sum signal and the difference signal, a test signal having a known amplitude / phase characteristic sent from the third system is injected into the first system and the second system, and the first system and the second system are injected. Whether the power feeding system has changed due to changes in installation conditions, etc., by detecting the amplitude and phase differences of the signals between the systems using the system test signals and comparing them with the reference values held in advance. In the case of a change, the amplitude and phase characteristics of the test signal between systems due to the change are automatically compensated.

従って、新たに信号系統を設けたり、特別な測定器等を用いることなく、給電系が変化した場合において、各チャンネル間の振幅・位相特性の調整を自動で行うことが可能となり、これにより運用における長期間の安定度の確保が可能となる。   Therefore, it is possible to automatically adjust the amplitude and phase characteristics between each channel when the power supply system changes without providing a new signal system or using special measuring instruments. It is possible to ensure long-term stability.

以上詳述したようにこの発明によれば、給電系が変化した場合において、各チャンネル間の振幅・位相特性の調整を自動で行うことが可能となり、これにより運用における長期間の安定度の確保が可能な二次監視レーダ装置を提供することができる。   As described above in detail, according to the present invention, it is possible to automatically adjust the amplitude and phase characteristics between the channels when the power feeding system changes, thereby ensuring long-term stability in operation. Therefore, it is possible to provide a secondary monitoring radar device capable of performing

以下、この発明の実施形態について図面を参照して詳細に説明する。
まず、この発明に係る実施形態を説明するに先立ち、その動作原理について説明する。
Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings.
First, prior to describing an embodiment according to the present invention, an operation principle thereof will be described.

図1は、二次監視レーダ装置のモノパルス測角の原理を示す信号特性図である。   FIG. 1 is a signal characteristic diagram showing the principle of monopulse angle measurement of the secondary monitoring radar apparatus.

二次監視レーダ装置のモノパルス測角方式における、モノパルス信号からターゲット(図1中では1T、2T、3Tを示す)の方位を測定する処理では、複数エレメントの受信信号を加算した和パターンΣと減算した差パターンΔを生成し、その和パターンΣと差パターンΔの振幅値からオフボアサイト角の計算を行い、受信ビームの中心からのターゲット方位のずれを求めている。   In the monopulse angle measurement method of the secondary monitoring radar apparatus, in the process of measuring the azimuth of the target (showing 1T, 2T, and 3T in FIG. 1) from the monopulse signal, a sum pattern Σ obtained by adding the reception signals of a plurality of elements is subtracted. The difference pattern Δ is generated, the off-bore sight angle is calculated from the sum pattern Σ and the amplitude value of the difference pattern Δ, and the deviation of the target orientation from the center of the received beam is obtained.

例えば図1(a)に示すように、受信ビームの中心にターゲット2Tがいるときは、和パターンΣが最大の振幅となり、差パターンΔの振幅が最小になる。また、振幅差は、図1(b)に示すように、最大となる。さらに、位相差は、図1(c)に示すように、ゼロとなる。   For example, as shown in FIG. 1A, when the target 2T is at the center of the reception beam, the sum pattern Σ has the maximum amplitude and the difference pattern Δ has the minimum amplitude. Further, the amplitude difference becomes maximum as shown in FIG. Further, the phase difference becomes zero as shown in FIG.

また、中心からx°傾く場合では、和パターンΣの振幅は中心時の振幅より小さくなり、差パターンΔの振幅はαになり、差パターンΔと和パターンΣの比率を計算し中心からのずれx°を求めている。   When the angle is tilted by x ° from the center, the amplitude of the sum pattern Σ is smaller than the amplitude at the center, the amplitude of the difference pattern Δ is α, the ratio of the difference pattern Δ and the sum pattern Σ is calculated, and the deviation from the center x ° is obtained.

上記の原理に基づき、以下にこの発明の実施形態について説明する。   Based on the above principle, an embodiment of the present invention will be described below.

(第1の実施形態)
図2は、この発明に係る二次監視レーダ装置の第1の実施形態の構成を示すブロック図である。図2において、送信機1から例えばターゲットとなる航空機(図示せず)の識別を行なうために必要なINT(インタロゲーション)送信信号が発生される。このINT送信信号は、サーキュレータ2を介して空中線装置3により航空機に向けて送出される。
(First embodiment)
FIG. 2 is a block diagram showing the configuration of the first embodiment of the secondary monitoring radar apparatus according to the present invention. In FIG. 2, an INT (interrogation) transmission signal necessary for identifying, for example, a target aircraft (not shown) is generated from the transmitter 1. This INT transmission signal is sent to the aircraft by the antenna device 3 through the circulator 2.

そして、航空機のトランスポンダから上記INT送信信号に対する応答信号が空中線装置3で受信される。空中線装置3は、複数エレメントにおける各受信信号を加算して和パターンΣのRF(無線周波数)信号を生成し、各受信信号を減算して差パターンΔのRF信号を生成する。   Then, a response signal to the INT transmission signal is received by the antenna device 3 from the transponder of the aircraft. The antenna device 3 adds the received signals in the plurality of elements to generate an RF (radio frequency) signal of the sum pattern Σ, and subtracts the received signals to generate an RF signal of the difference pattern Δ.

上記空中線装置3で得られた和パターンΣのRF信号はサーキュレータ2を介して受信機4に供給され、差パターンのRF信号は直接受信機4に供給される。   The sum pattern Σ RF signal obtained by the antenna apparatus 3 is supplied to the receiver 4 via the circulator 2, and the difference pattern RF signal is supplied directly to the receiver 4.

一方、送信機1から発生されるオムニパターンのSLS(サイドローブ・サプレッション)送信信号は、サーキュレータ6を介して空中線装置3にて航空機に向けて送出され、空中線装置3にて得られたオムニパターンのRF信号は、サーキュレータ6を介して受信機4に供給される。このオムニパターンのSLS送信信号は、INT送信信号に対する誤応答を防止するための信号である。   On the other hand, an omni-pattern SLS (sidelobe suppression) transmission signal generated from the transmitter 1 is sent to the aircraft by the antenna device 3 via the circulator 6, and the omni pattern obtained by the antenna device 3 is obtained. The RF signal is supplied to the receiver 4 via the circulator 6. The omni-pattern SLS transmission signal is a signal for preventing an erroneous response to the INT transmission signal.

各RF信号(和パターンΣ、差パターンΔ、オムニパターン)は、受信機4で増幅、周波数変換が行われてIF(中間周波数)信号となり、信号処理部5に入力される。信号処理部5で処理が施された和パターンΣ及び差パターンΔは、目標処理部9に供給される。   Each RF signal (sum pattern Σ, difference pattern Δ, omni pattern) is amplified and frequency converted by the receiver 4 to become an IF (intermediate frequency) signal, which is input to the signal processing unit 5. The sum pattern Σ and the difference pattern Δ processed by the signal processing unit 5 are supplied to the target processing unit 9.

上記目標処理部9は、和パターンΣ及び差パターンΔからオフポアサイト角つまりターゲット方向を検出する。また、目標処理部9には、オムニパターンのIF信号が供給され、ターゲットからの誤応答の防止に供される。   The target processing unit 9 detects an off-pore site angle, that is, a target direction from the sum pattern Σ and the difference pattern Δ. The target processing unit 9 is supplied with an omni-pattern IF signal to prevent erroneous responses from the target.

ところで、本実施形態に係る信号処理部5には、各チャンネル間(和パターンΣ、差パターンΔ)の振幅/位相特性を調整するための振幅/位相調整回路11と、各チャンネル間(和パターンΣ、差パターンΔ)の振幅/位相の相対差を検出する振幅/位相検出回路12と、予め各チャンネル間(和パターンΣ、差パターンΔ)の振幅/位相が一意に定まる基準値を保持する保持部13と、振幅/位相検出回路12の検出結果と保持部13に保持される基準値とを比較する比較回路14とを備えている。   By the way, the signal processing unit 5 according to the present embodiment includes an amplitude / phase adjustment circuit 11 for adjusting the amplitude / phase characteristics between the channels (sum pattern Σ, difference pattern Δ), and between the channels (sum pattern). An amplitude / phase detection circuit 12 that detects a relative difference in amplitude / phase of Σ and difference pattern Δ, and a reference value that uniquely determines the amplitude / phase of each channel (sum pattern Σ, difference pattern Δ) in advance. A holding unit 13 and a comparison circuit 14 that compares the detection result of the amplitude / phase detection circuit 12 with a reference value held in the holding unit 13 are provided.

また、オムニパターンの給電系には、パイロット信号発生回路7が設けられ、さらに空中線装置3と受信機4との間には、パイロット信号注入回路8が設けられる。パイロット信号発生回路7は、和パターンΣ及び差パターンΔに対し既知の振幅・位相特性を有するパイロット信号を発生する。このパイロット信号は、パイロット信号注入回路8により和パターンΣ及び差パターンΔそれぞれの給電系に注入されることになる。   In addition, a pilot signal generation circuit 7 is provided in the omni-pattern feeding system, and a pilot signal injection circuit 8 is provided between the antenna device 3 and the receiver 4. The pilot signal generation circuit 7 generates a pilot signal having known amplitude / phase characteristics with respect to the sum pattern Σ and the difference pattern Δ. This pilot signal is injected by the pilot signal injection circuit 8 into the feeding systems of the sum pattern Σ and the difference pattern Δ.

上記構成において、以下にその特徴となる処理動作について説明する。
以前に考えられていた二次監視レーダ装置では、図3に示すように、空中線装置3にて受信された各RF信号(和パターンΣ、差パターンΔ)は、受信機4に入力され受信信号の増幅、周波数変換が行われ、目標処理部21に入力される。
In the above-described configuration, processing operations that are characteristic of the configuration will be described below.
In the secondary monitoring radar apparatus considered before, as shown in FIG. 3, each RF signal (sum pattern Σ, difference pattern Δ) received by the antenna apparatus 3 is input to the receiver 4 to receive signals. Amplification and frequency conversion are performed and input to the target processing unit 21.

目標処理部21では、各チャンネル間(和パターンΣ、差パターンΔ)の振幅/位相の相対差からモノパルス測角テーブルを作成し、航空機からの各受信信号をもとにモノパルス測角テーブルを参照することにより航空機の方位を決定する。   The target processing unit 21 creates a monopulse angle measurement table from the relative amplitude / phase differences between the channels (sum pattern Σ, difference pattern Δ), and refers to the monopulse angle measurement table based on each received signal from the aircraft. To determine the orientation of the aircraft.

適切なモノパルス測角を行うため振幅/位相調整回路22にて、和パターンΣ、差パターンΔについて振幅/位相特性の調整を行う。   In order to perform appropriate monopulse angle measurement, the amplitude / phase characteristics are adjusted by the amplitude / phase adjustment circuit 22 for the sum pattern Σ and the difference pattern Δ.

従来の回路方式では、設置条件の変更等により給電系が変化した場合には、振幅/位相調整回路22にて再調整が必要である。この調整は、人為的作業によって行なわれるため、手間及び時間を多く費やすことになる。   In the conventional circuit system, readjustment is required by the amplitude / phase adjustment circuit 22 when the power supply system changes due to a change in installation conditions or the like. Since this adjustment is performed by human work, it takes a lot of time and effort.

そこで、本実施形態では、和パターンΣ及び差パターンΔに対し既知の振幅・位相特性を有するパイロット信号を利用して、給電系が変化した場合にチャンネル間の振幅・位相特性を自動で調整できるようにした。   Therefore, in this embodiment, the pilot signal having known amplitude / phase characteristics with respect to the sum pattern Σ and the difference pattern Δ can be used to automatically adjust the amplitude / phase characteristics between channels when the power feeding system changes. I did it.

図4(a)は送信機1で生成される送信信号、図4(b)はパイロット信号発生回路7で生成されるパイロット信号、図4(c)、(d)は空中線装置3で得られる和パターンΣ、差パターンΔの例を示すものである。   4A is a transmission signal generated by the transmitter 1, FIG. 4B is a pilot signal generated by the pilot signal generation circuit 7, and FIGS. 4C and 4D are obtained by the antenna apparatus 3. An example of the sum pattern Σ and the difference pattern Δ is shown.

適切なモノパルス測角を行うため、和パターンΣ、差パターンΔについて振幅・位相特性の調整を行うが、これは試験用送信装置からの受信信号を基に、信号処理部5の振幅/位相調整回路11にて調整を行う。調整後における各チャンネル間(和パターンΣ、差パターンΔ)の振幅/位相の相対差は、振幅/位相検出回路12にて検出され、その結果を初期値とし保持部13に保存する。   In order to perform appropriate monopulse angle measurement, the amplitude and phase characteristics of the sum pattern Σ and the difference pattern Δ are adjusted. This is based on the received signal from the test transmission device, and the amplitude / phase adjustment of the signal processing unit 5 is performed. Adjustment is performed by the circuit 11. The relative amplitude / phase difference between the channels (sum pattern Σ, difference pattern Δ) after adjustment is detected by the amplitude / phase detection circuit 12, and the result is stored in the holding unit 13 as an initial value.

基準値が設定された以降の振幅・位相特性の調整は、パイロット信号発生回路7からのパイロット信号について各チャンネル間(和パターンΣ、差パターンΔ)の振幅・位相の相対差を検出し、比較回路14にて基準値との比較を行う。比較した結果、基準値との差が生じている場合には、振幅/位相調整回路11に対し基準値との差が0となるまで制御信号、つまり基準値との差に相当する補償量が出力される。   Adjustment of the amplitude / phase characteristics after the reference value is set is performed by detecting the relative difference in amplitude / phase between the channels (sum pattern Σ, difference pattern Δ) of the pilot signal from the pilot signal generation circuit 7 and comparing it. The circuit 14 compares with the reference value. If there is a difference from the reference value as a result of the comparison, the compensation amount corresponding to the difference from the control signal, that is, the reference value, is kept until the difference from the reference value becomes zero for the amplitude / phase adjustment circuit 11. Is output.

振幅/位相調整回路11は、各チャンネルのパイロット信号と制御信号(補償量)とを入力し、制御信号に従って各チャンネルのパイロット信号の振幅・位相特性を補償し、補償後のパイロット信号を目標処理部9及び振幅/位相検出回路12に出力する。   The amplitude / phase adjustment circuit 11 receives a pilot signal of each channel and a control signal (compensation amount), compensates the amplitude / phase characteristics of the pilot signal of each channel according to the control signal, and performs target processing on the compensated pilot signal. To the unit 9 and the amplitude / phase detection circuit 12.

以上のように上記実施形態では、空中線装置3で得られる和パターンΣ及び差パターンΔに代えて、オムニパターンの給電系上のパイロット信号発生回路7で生成される既知の振幅・位相特性を有するパイロット信号をパイロット注入回路8にて和パターンΣのチャンネル及び差パターンΔのチャンネルに注入し、これらチャンネルのパイロット信号を利用して、振幅/位相検出回路12にて各チャンネル間の信号の振幅差及び位相差を検出し、比較回路14にて予め保持部13に保持されている基準値と比較することで、設置条件の変更等により給電系が変化したか否かを判断し、変化した場合には、変化したことによるチャンネル間の信号の振幅・位相特性を自動で調整するようにしている。   As described above, in the above-described embodiment, instead of the sum pattern Σ and the difference pattern Δ obtained by the antenna apparatus 3, a known amplitude / phase characteristic generated by the pilot signal generation circuit 7 on the omni-pattern feeding system is provided. The pilot signal is injected into the channel of the sum pattern Σ and the channel of the difference pattern Δ by the pilot injection circuit 8, and the amplitude difference of the signal between the channels is detected by the amplitude / phase detection circuit 12 using the pilot signals of these channels. And the phase difference is detected and compared with a reference value held in the holding unit 13 in advance by the comparison circuit 14 to determine whether or not the power feeding system has changed due to a change in installation conditions or the like. For example, the amplitude / phase characteristics of signals between channels due to the change are automatically adjusted.

従って、新たに給電系を設けたり、特別な測定器等を用いることなく、給電系が変化した場合において、各チャンネル間の振幅・位相特性の調整を自動で行うことが可能となり、これにより運用における長期間の安定度の確保が可能となる。   Therefore, it is possible to automatically adjust the amplitude and phase characteristics between each channel when the power supply system changes without installing a new power supply system or using a special measuring instrument. It is possible to ensure long-term stability.

また、信号処理部5は、振幅/位相調整回路11、振幅/位相検出回路12、保持部13及び比較回路14をデジタル処理により実現することで、経年変化にも対応できる。   Further, the signal processing unit 5 can cope with aging by realizing the amplitude / phase adjustment circuit 11, the amplitude / phase detection circuit 12, the holding unit 13 and the comparison circuit 14 by digital processing.

(第2の実施形態)
図5は、二次監視レーダ装置の第2の実施形態の構成を示すものである。なお、図5において、上記図2と同一部分には同一符号を付して、詳細な説明を省略する。
(Second Embodiment)
FIG. 5 shows the configuration of the second embodiment of the secondary monitoring radar apparatus. In FIG. 5, the same parts as those in FIG. 2 are denoted by the same reference numerals, and detailed description thereof is omitted.

この二次監視レーダ装置では、第1の実施形態が振幅/位相調整回路11の出力を振幅/位相検出回路12に入力していたのに対し、受信機4の出力を振幅/位相検出回路12に入力するようにしている。   In this secondary monitoring radar apparatus, the output of the receiver 4 is input to the amplitude / phase detection circuit 12 while the output of the amplitude / phase adjustment circuit 11 is input to the amplitude / phase detection circuit 12 in the first embodiment. To enter.

(その他の実施形態)
なお、この発明は、上記各実施形態に限定されるものではない。例えば、パイロット信号注入回路にて適切な信号レベルに設定することにより、パイロット信号発生回路から発生されるパイロット信号に代えて、SLS送信信号を基準信号として使用することも可能である。この場合、パイロット信号注入回路にてSLS送信信号を和パターンのチャンネル及び差パターンのチャンネルにそれぞれ注入することになる。
(Other embodiments)
The present invention is not limited to the above embodiments. For example, by setting an appropriate signal level in the pilot signal injection circuit, it is possible to use the SLS transmission signal as a reference signal instead of the pilot signal generated from the pilot signal generation circuit. In this case, the SLS transmission signal is injected into the sum pattern channel and the difference pattern channel by the pilot signal injection circuit.

さらに、実施段階ではその要旨を逸脱しない範囲で構成要素を変形して具体化できる。また、上記実施形態に開示されている複数の構成要素の適宜な組み合わせにより、種々の発明を形成できる。例えば、実施形態に示される全構成要素から幾つかの構成要素を削除してもよい。   Furthermore, in the implementation stage, the constituent elements can be modified and embodied without departing from the spirit of the invention. In addition, various inventions can be formed by appropriately combining a plurality of components disclosed in the embodiment. For example, some components may be deleted from all the components shown in the embodiment.

この発明に係わる二次監視レーダ装置のモノパルス測角の原理を示す信号特性図。The signal characteristic figure which shows the principle of the monopulse angle measurement of the secondary monitoring radar apparatus concerning this invention. この発明に係わる二次監視レーダ装置の第1の実施形態を示すブロック図。The block diagram which shows 1st Embodiment of the secondary monitoring radar apparatus concerning this invention. 以前に考えられた二次監視レーダ装置の構成を示すブロック図。The block diagram which shows the structure of the secondary monitoring radar apparatus considered before. 同第1の実施形態における送信信号、パイロット信号、和パターン及び差パターンの波形を示す図。The figure which shows the waveform of the transmission signal, pilot signal, sum pattern, and difference pattern in the said 1st Embodiment. この発明に係わる二次監視レーダ装置の第2の実施形態を示すブロック図。The block diagram which shows 2nd Embodiment of the secondary monitoring radar apparatus concerning this invention.

符号の説明Explanation of symbols

1…送信機、2,6…サーキュレータ、3…空中線装置、4…受信機、5…信号処理部、7…パイロット信号発生回路、8…パイロット信号注入回路、9…目標処理部、11…振幅/位相調整回路、12…振幅/位相検出回路、13…保持部、14…比較回路。   DESCRIPTION OF SYMBOLS 1 ... Transmitter, 2 and 6 ... Circulator, 3 ... Antenna apparatus, 4 ... Receiver, 5 ... Signal processing part, 7 ... Pilot signal generation circuit, 8 ... Pilot signal injection circuit, 9 ... Target processing part, 11 ... Amplitude / Phase adjustment circuit, 12 ... amplitude / phase detection circuit, 13 ... holding unit, 14 ... comparison circuit.

Claims (5)

目標対象物からの第1の信号を空中線装置にて受信し、前記空中線装置の複数エレメントで得られる各受信信号の和信号を第1系統へ、各受信信号の差信号を第2系統へ分岐して目標処理部に入力すると共に、前記目標対象物と前記目標処理部との間で前記第1の信号に対する誤応答を防止するための第2の信号を第3系統を介して送受信し、前記目標処理部にて前記和信号、前記差信号及び前記第2の信号から前記目標対象物に関する目標情報を得る二次監視レーダ装置において、
前記第3系統に設けられ、前記和信号及び前記差信号に対しそれぞれ既知の振幅・位相特性を有する試験信号を発生する試験信号発生手段と、
前記試験信号送出時に、前記和信号及び前記差信号に代わって前記試験信号を前記第1及び第2系統に注入する試験信号注入手段と、
前記試験信号送出時に、前記第1及び第2系統間の試験信号の振幅差及び位相差を検出する検出手段と、
この検出手段による検出結果から補償量を求める補償量演算手段と、
この補償量演算手段で得られた補償量に基づいて、前記第1及び第2系統間の試験信号の振幅・位相特性を補償して前記目標処理部に出力する補償手段とを具備したことを特徴とする二次監視レーダ装置。
The first signal from the target object is received by the antenna device, and the sum signal of each received signal obtained by the plurality of elements of the antenna device is branched to the first system, and the difference signal of each received signal is branched to the second system And input and output to the target processing unit via the third system a second signal for preventing an erroneous response to the first signal between the target object and the target processing unit, In the secondary monitoring radar device that obtains target information about the target object from the sum signal, the difference signal, and the second signal in the target processing unit,
Test signal generating means provided in the third system for generating a test signal having known amplitude and phase characteristics for the sum signal and the difference signal,
Test signal injection means for injecting the test signal into the first and second systems in place of the sum signal and the difference signal when the test signal is transmitted;
Detecting means for detecting an amplitude difference and a phase difference of the test signal between the first and second systems when the test signal is transmitted;
Compensation amount calculating means for obtaining a compensation amount from the detection result by the detecting means;
Compensation means for compensating for the amplitude / phase characteristics of the test signal between the first and second systems based on the compensation amount obtained by the compensation amount computing means and outputting to the target processing unit. A secondary monitoring radar device.
目標対象物からの第1の信号を空中線装置にて受信し、前記空中線装置の複数エレメントで得られる各受信信号の和信号を第1系統へ、各受信信号の差信号を第2系統へ分岐して目標処理部に入力すると共に、前記目標対象物と前記目標処理部との間で前記第1の信号に対する誤応答を防止するための第2の信号を第3系統を介して送受信し、前記目標処理部にて前記和信号、前記差信号及び前記第2の信号から前記目標対象物に関する目標情報を得る二次監視レーダ装置において、
前記第3系統に設けられ、前記和信号及び前記差信号に対しそれぞれ既知の振幅・位相特性を有する試験信号を発生する試験信号発生手段と、
前記試験信号送出時に、前記和信号及び前記差信号に代わって前記試験信号を前記第1及び第2系統に注入する試験信号注入手段と、
この試験信号注入手段で得られた試験信号を入力し、与えられる補償量に基づいて前記第1及び第2系統間の試験信号の振幅・位相特性を補償して前記目標処理部に出力する補償手段と、
この補償手段で補償処理された第1及び第2系統間の試験信号の振幅差及び位相差を検出する検出手段と、
この検出手段による検出結果から、前記補償手段に与える補償量を求める補償量演算手段とを具備したことを特徴とする二次監視レーダ装置。
The first signal from the target object is received by the antenna device, and the sum signal of each received signal obtained by the plurality of elements of the antenna device is branched to the first system, and the difference signal of each received signal is branched to the second system And input and output to the target processing unit via the third system a second signal for preventing an erroneous response to the first signal between the target object and the target processing unit, In the secondary monitoring radar device that obtains target information about the target object from the sum signal, the difference signal, and the second signal in the target processing unit,
Test signal generating means provided in the third system for generating a test signal having known amplitude and phase characteristics for the sum signal and the difference signal,
Test signal injection means for injecting the test signal into the first and second systems in place of the sum signal and the difference signal when the test signal is transmitted;
Compensation for inputting the test signal obtained by the test signal injection means, compensating the amplitude / phase characteristics of the test signal between the first and second systems based on the given compensation amount, and outputting the compensation to the target processing unit Means,
Detecting means for detecting the amplitude difference and phase difference of the test signal between the first and second systems compensated by the compensating means;
A secondary monitoring radar apparatus comprising: a compensation amount calculation means for obtaining a compensation amount to be given to the compensation means from a detection result by the detection means.
目標対象物からの第1の信号を空中線装置にて受信し、前記空中線装置の複数エレメントで得られる各受信信号の和信号を第1系統へ、各受信信号の差信号を第2系統へ分岐して目標処理部に入力すると共に、前記目標対象物と前記目標処理部との間で前記第1の信号に対する誤応答を防止するための第2の信号を第3系統を介して送受信し、前記目標処理部にて前記和信号、前記差信号及び前記第2の信号から前記目標対象物に関する目標情報を得る二次監視レーダ装置において、
前記和信号及び前記差信号に代わって前記第2の信号を前記第1及び第2系統に注入する注入手段と、
前記第1及び第2系統間の信号の振幅差及び位相差を検出する検出手段と、
この検出手段による検出結果から補償量を求める補償量演算手段と、
この補償量演算手段で得られた補償量に基づいて、前記第1及び第2系統間の信号の振幅・位相特性を補償して前記目標処理部に出力する補償手段とを具備したことを特徴とする二次監視レーダ装置。
The first signal from the target object is received by the antenna device, and the sum signal of each received signal obtained by the plurality of elements of the antenna device is branched to the first system, and the difference signal of each received signal is branched to the second system And input and output to the target processing unit via the third system a second signal for preventing an erroneous response to the first signal between the target object and the target processing unit, In the secondary monitoring radar device that obtains target information about the target object from the sum signal, the difference signal, and the second signal in the target processing unit,
Injection means for injecting the second signal into the first and second systems instead of the sum signal and the difference signal;
Detecting means for detecting an amplitude difference and a phase difference of signals between the first and second systems;
Compensation amount calculating means for obtaining a compensation amount from the detection result by the detecting means;
Compensating means for compensating for the amplitude / phase characteristics of the signal between the first and second systems based on the compensation amount obtained by the compensation amount computing means and outputting to the target processing section. A secondary monitoring radar device.
目標対象物からの第1の信号を空中線装置にて受信し、前記空中線装置の複数エレメントで得られる各受信信号の和信号を第1系統へ、各受信信号の差信号を第2系統へ分岐して目標処理部に入力すると共に、前記目標対象物と前記目標処理部との間で前記第1の信号に対する誤応答を防止するための第2の信号を第3系統を介して送受信し、前記目標処理部にて前記和信号、前記差信号及び前記第2の信号から前記目標対象物に関する目標情報を得る二次監視レーダ装置において、
前記和信号及び前記差信号に代わって前記第2の信号を前記第1及び第2系統に注入する注入手段と、
この注入手段で得られた信号を入力し、与えられる補償量に基づいて前記第1及び第2系統間の信号の振幅・位相特性を補償して前記目標処理部に出力する補償手段と、
この補償手段で補償処理された第1及び第2系統間の信号の振幅差及び位相差を検出する検出手段と、
この検出手段による検出結果から、前記補償手段に与える補償量を求める補償量演算手段とを具備したことを特徴とする二次監視レーダ装置。
The first signal from the target object is received by the antenna device, and the sum signal of each received signal obtained by the plurality of elements of the antenna device is branched to the first system, and the difference signal of each received signal is branched to the second system And input to the target processing unit, and transmits and receives the second signal for preventing an erroneous response to the first signal between the target object and the target processing unit via the third system, In the secondary monitoring radar device that obtains target information about the target object from the sum signal, the difference signal, and the second signal in the target processing unit,
Injection means for injecting the second signal into the first and second systems instead of the sum signal and the difference signal;
Compensation means for inputting the signal obtained by the injection means, compensating for the amplitude / phase characteristics of the signal between the first and second systems based on a given compensation amount, and outputting to the target processing section;
Detecting means for detecting an amplitude difference and a phase difference of signals between the first and second systems compensated by the compensating means;
A secondary monitoring radar apparatus comprising: a compensation amount calculation means for obtaining a compensation amount to be given to the compensation means from a detection result by the detection means.
前記補償量演算手段は、予め前記和信号と前記差信号との振幅差及び位相差が一意に定まる基準値を保持する基準値保持手段と、前記検出手段で検出される振幅差及び位相差と前記基準値保持手段で保持されている基準値とを比較することで、前記補償量を求める比較手段とを備えることを特徴とする請求項1乃至4の少なくとも1つに記載の二次監視レーダ装置。 The compensation amount calculating means includes a reference value holding means for holding a reference value that uniquely determines an amplitude difference and a phase difference between the sum signal and the difference signal in advance, and an amplitude difference and a phase difference detected by the detecting means. 5. The secondary monitoring radar according to claim 1, further comprising: a comparison unit that obtains the compensation amount by comparing the reference value held by the reference value holding unit. apparatus.
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Publication number Priority date Publication date Assignee Title
JP2019503491A (en) * 2016-02-12 2019-02-07 ローベルト ボッシュ ゲゼルシャフト ミット ベシュレンクテル ハフツング Radar sensor for car driver assist system
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JP2007078463A (en) * 2005-09-13 2007-03-29 Toshiba Corp Monitoring radar equipment

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JP2019503491A (en) * 2016-02-12 2019-02-07 ローベルト ボッシュ ゲゼルシャフト ミット ベシュレンクテル ハフツング Radar sensor for car driver assist system
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RU2725418C1 (en) * 2019-02-15 2020-07-02 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Monopulse radar system with high accuracy of determining target bearing angle
US11320528B1 (en) 2019-11-20 2022-05-03 Telephonics Corporation Monopulse secondary surveillance radar system

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