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JPS636835B2 - - Google Patents
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JPS636835B2 - - Google Patents

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Publication number
JPS636835B2
JPS636835B2 JP55006974A JP697480A JPS636835B2 JP S636835 B2 JPS636835 B2 JP S636835B2 JP 55006974 A JP55006974 A JP 55006974A JP 697480 A JP697480 A JP 697480A JP S636835 B2 JPS636835 B2 JP S636835B2
Authority
JP
Japan
Prior art keywords
circuit
signal
output signal
output
radar
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
JP55006974A
Other languages
Japanese (ja)
Other versions
JPS56104265A (en
Inventor
Juichi Okabe
Katsuzo Tsukada
Masao Chiba
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.)
Toshiba Corp
Original Assignee
Tokyo Shibaura Electric Co 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 Tokyo Shibaura Electric Co Ltd filed Critical Tokyo Shibaura Electric Co Ltd
Priority to JP697480A priority Critical patent/JPS56104265A/en
Publication of JPS56104265A publication Critical patent/JPS56104265A/en
Publication of JPS636835B2 publication Critical patent/JPS636835B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/50Systems of measurement based on relative movement of target
    • G01S13/52Discriminating between fixed and moving objects or between objects moving at different speeds
    • G01S13/522Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves
    • G01S13/524Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi
    • G01S13/526Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi performing filtering on the whole spectrum without loss of range information, e.g. using delay line cancellers or comb filters

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar Systems Or Details Thereof (AREA)

Description

【発明の詳細な説明】 本発明は雨、雪等の気象情報をレーダにより定
量的に測定する気象レーダ装置等に適用して気象
情報に山岳、草木、建物等の不要情報、いわゆる
グランドクラツタが重量した場合でも、不要情報
を除去し、気象情報のみを的確に抽出し得るレー
ダ信号処理装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention is applied to a weather radar device that quantitatively measures meteorological information such as rain and snow using a radar, and eliminates unnecessary information such as mountains, plants, buildings, etc., so-called grand clutter. The present invention relates to a radar signal processing device that can remove unnecessary information and accurately extract only weather information even when the weather is heavy.

周知の様に、従来航空管制用レーダに於いて、
グランドクラツタ等不要情報を除去し、航空機等
の目標情報のみを抽出する方式に移動目標指示方
式、いわゆるMTI方式があり、これは、レーダ
送信パルス毎の受信信号の相関関係に注目し、グ
ランドクラツタ等の固定目標を消去する機能を有
している。
As is well known, in conventional air traffic control radar,
There is a moving target indication method, so-called MTI method, which removes unnecessary information such as ground clutter and extracts only target information such as aircraft. It has a function to erase fixed targets such as clutter.

気象レーダに於いても、グランドクラツタを除
去し気象情報のみを抽出するには、グランドクラ
ツタ等の固定目標と気象情報間に於ける受信信号
のレーダ送信パルス毎の相関関係の違いに注目す
ることにより、上記MTI方式を利用して定量的
な気象情報の測定が可能なことが知られている。
In the case of weather radar, in order to remove ground clutter and extract only weather information, it is necessary to pay attention to the difference in the correlation of each radar transmission pulse of the received signal between fixed targets such as ground clutter and weather information. It is known that quantitative weather information can be measured by using the above MTI method.

さて、通常の気象レーダは非常に広範囲の振幅
レベルを持つ気象情報を飽和することなく表示し
また測定するために受信機受信回路に対数特性の
ものを使用している。そこでこの受信機信号処理
段に於いて、MTI方式を採用し定量的気象情報
の測定を行うためには、一旦対数一直線変換し、
直線特性でのMTI方式にする必要がある。
Now, a typical weather radar uses a receiver receiving circuit having a logarithmic characteristic in order to display and measure weather information having a very wide range of amplitude levels without saturation. Therefore, in order to measure quantitative weather information by adopting the MTI method in this receiver signal processing stage, logarithmically linear transformation is performed,
It is necessary to use the MTI method with linear characteristics.

つまり、対数特性受信回路からのレーダ送信パ
ルス毎のグランドクラツタの受信電力を10logPg
(t)、10logPg(t−T)、…、10logPg(t−nT)、
又気象情報の受信電力を10logPr(t)、10logPr(t
−T)、…、10logPr(t−nT)、又グランドクラ
ツタと気象情報が重畳した受信電力を10log(Pr
+Pg)(t)、10log(Pr+Pg)(t−T)、…、10log
(Pr+Pg)(t−nT)とすると、各々を対数一直
線変換し、Pg(t)、Pg(t−T)、…、Pg(t−
nT)、又、Pr(t)、Pr(t−T)、…、Pr(t−
nT)、又、(Pr+Pg)(t)、(Pr+Pg)(t−T)、
…、(Pr+Pg)(t−nT)を得る。これらの信号
をMTI回路を通すことにより、グランドクラツ
タのみの場合は、Pg(t)とPg(t−T)間の相関係
数が1に近くなりMTI回路出力はほぼ零となる。
従つて、グランドクラツタと気象情報が重畳した
場合には、MTI回路出力は(Pr+Pg)(t)−(Pr
+Pg)(t−T)=Pr(t)−Pr(t−T)となり、気
象情報のみを抽出することができる。
In other words, the received power of the ground clutter for each radar transmission pulse from the logarithmic characteristic receiving circuit is 10logPg.
(t), 10logPg (t-T), ..., 10logPg (t-nT),
Also, the received power of weather information is 10logPr(t), 10logPr(t
−T), ..., 10logPr(t-nT), and the received power with ground clutter and weather information superimposed is 10log(Pr
+Pg)(t), 10log(Pr+Pg)(t-T),..., 10log
(Pr+Pg)(t-nT), each is transformed into a logarithm, and Pg(t), Pg(t-T),..., Pg(t-
nT), also Pr(t), Pr(t-T), ..., Pr(t-
nT), (Pr+Pg)(t), (Pr+Pg)(t-T),
..., (Pr+Pg)(t-nT) is obtained. By passing these signals through the MTI circuit, in the case of only ground clutter, the correlation coefficient between Pg(t) and Pg(t-T) approaches 1, and the MTI circuit output becomes almost zero.
Therefore, when ground clutter and weather information are superimposed, the MTI circuit output is (Pr + Pg) (t) - (Pr
+Pg)(t-T)=Pr(t)-Pr(t-T), and only weather information can be extracted.

しかし、実際には、グランドクラツタは風等の
影響あるいは、受信機雑音が重畳することによ
り、少なからず変動している。この変動成分は、
対数特性受信回路を用いることにより、かなり圧
縮されてはいるが、MTI回路入力段で対数一直
線変換することにより、MTI回路出力段では大
きな変動成分として検出され気象情報の測定に多
大な影響を及ぼしていた。
However, in reality, ground clutter fluctuates to a large extent due to the influence of wind, etc., or due to the superposition of receiver noise. This fluctuation component is
Although it is considerably compressed by using a logarithmic characteristic receiving circuit, by performing logarithmic linear transformation at the MTI circuit input stage, it is detected as a large fluctuation component at the MTI circuit output stage, which has a great influence on the measurement of weather information. was.

従来のこのレーダ信号処理装置の構成を第1図
を参照して説明する。即ち、空中線1で捕捉され
たレーダ目標反射信号は受信機内の例えば対数増
幅器からなる対数特性受信回路2を経て量子化回
路3に供給される。量子化回路3は例えばいわゆ
るA―D変換器で構成され、距離サンプリング信
号ごとに振幅方向に量子化されたデイジタル信号
を導出する。次に、この量子化回路3出力信号を
対数一直線変換回路4により直線特性信号に変換
し、この出力信号とレーダの1送信繰返し時間遅
延を与える遅延回路5出力信号とを減算回路6に
導入して両出力信号の変動成分を抽出する。次
に、この減算回路6出力信号を直線一対数変換回
路7により対数特性信号に変換し、従来の気象レ
ーダと同様な対数信号を得る。第2図は第1図に
示した装置の信号波形図であり、波形aは対数特
性受信回路2の出力信号波形、波形bは直線一対
数変換回路7の出力信号波形である。又、波形
a,bにおいて21は変動成分が重畳したグラン
ドクラツタ、22は雨、23は雑音をそれぞれ示
している。第1図に示した従来装置では第2図波
形aに示した対数特性受信回路2出力信号のグラ
ンドクラツタ及びそれに重畳した微弱な変動成分
21は、直線一対数変換回路7においては大きな
変動成分(第2図波形bにおける24)として検
出され、気象情報との識別が困難である。
The configuration of this conventional radar signal processing device will be explained with reference to FIG. That is, the radar target reflected signal captured by the antenna 1 is supplied to the quantization circuit 3 via a logarithmic characteristic receiving circuit 2, which is comprised of, for example, a logarithmic amplifier, in the receiver. The quantization circuit 3 is composed of, for example, a so-called AD converter, and derives a digital signal quantized in the amplitude direction for each distance sampling signal. Next, this quantization circuit 3 output signal is converted into a linear characteristic signal by a logarithm-linear conversion circuit 4, and this output signal and a delay circuit 5 output signal that gives a one transmission repetition time delay of the radar are introduced into a subtraction circuit 6. The fluctuation components of both output signals are extracted. Next, the output signal of the subtraction circuit 6 is converted into a logarithmic characteristic signal by a linear-to-logarithmic conversion circuit 7 to obtain a logarithmic signal similar to that of a conventional weather radar. FIG. 2 is a signal waveform diagram of the apparatus shown in FIG. 1, in which waveform a is the output signal waveform of the logarithmic characteristic receiving circuit 2, and waveform b is the output signal waveform of the linear-to-logarithmic conversion circuit 7. Further, in waveforms a and b, 21 indicates ground clutter on which fluctuation components are superimposed, 22 indicates rain, and 23 indicates noise. In the conventional device shown in FIG. 1, the ground clutter and the weak fluctuation component 21 superimposed on the output signal of the logarithmic characteristic receiving circuit 2 shown in waveform a in FIG. (24 in waveform b in FIG. 2), and it is difficult to distinguish it from weather information.

本発明は、上記欠点に鑑みてなされたもので、
従来のレーダ信号処理装置のMTI方式における
気象情報の定量的測定能力を劣化させず、しかも
グランドクラツタ等の不要情報を効果的に除去す
るレーダ信号処理装置を提供するものである。
The present invention has been made in view of the above drawbacks, and
The object of the present invention is to provide a radar signal processing device that does not deteriorate the quantitative measurement ability of weather information in the MTI method of a conventional radar signal processing device and effectively removes unnecessary information such as ground clutter.

以下、本発明の一実施例を第3図を参照して詳
細に説明する。即ち、空中線31で捕捉された目
標反射信号は対数増幅器等からなる対数特性受信
回路32に供給される。対数特性受信回路32で
対数増幅等をなされた受信信号はA―D変換器等
の量子化回路33で距離サンプリング信号ごとに
振幅レベルがA―D変換される。いま、量子化回
路33の出力信号をAlogKP(t)とし、これを第1
図に示す従来装置のMTI回路に通すと、その出
力信号AlogK△P(t)は次のようになる。
Hereinafter, one embodiment of the present invention will be described in detail with reference to FIG. That is, the target reflected signal captured by the antenna 31 is supplied to a logarithmic characteristic receiving circuit 32 comprising a logarithmic amplifier or the like. The received signal that has been logarithmically amplified by the logarithmic characteristic receiving circuit 32 is subjected to A-to-D conversion of the amplitude level for each distance sampling signal by a quantization circuit 33 such as an A-to-D converter. Now, let the output signal of the quantization circuit 33 be Alog K P(t), and use this as the first
When passed through the MTI circuit of the conventional device shown in the figure, the output signal Alog K ΔP(t) is as follows.

AlogK△P(t)=AlogK{P(t)−P(t−T)}
………(1) また、この(1)式は、次のように変形される。
Alog K △P(t)=Alog K {P(t)−P(t−T)}
......(1) Also, this equation (1) can be transformed as follows.

AlogK△P(t)=AlogKP(t) +AlogK{1−P(t−T)/P(t)} ………(2) ここで、P(t)=KlogKP(t)、P(t−T)=
KlogKP(t-T)とおくと、上記(2)式は次のように置き
換えられる。
Alog K △P(t)=Alog K P(t) +Alog K {1-P(t-T)/P(t)} ......(2) Here, P(t)=K logKP(t) , P(t-T)=
By setting K logKP(tT) , the above equation (2) can be replaced as follows.

AlogK△P(t)=AlogKP(t) +AlogK〔1−K−{AlogKP(t) −AlogKP(t-T)}/A〕 ………(3) 本発明装置はこの(3)式を利用する。すなわち、
例えばA=10、K=10とし、かつ量子化回路33
出力信号を例えば10ビツトとすると、送信繰返し
ごとの出力信号10logP(t)、10logP(t−T)、…
は10ビツトのデイジタル信号として得られる。こ
の量子化回路33出力信号はレーダ送信繰返し時
間T遅延させる遅延回路34及び減算回路35に
それぞれ供給されることにより、減算回路35出
力信号は{10logP(t)−10logP(t−T)}となる。
Alog K △P(t)=Alog K P(t) +Alog K [1-K-{AlogKP(t) −AlogKP(tT)}/A] ......(3) The device of the present invention uses this formula (3) Take advantage of. That is,
For example, A=10, K=10, and the quantization circuit 33
For example, if the output signal is 10 bits, the output signal for each transmission repetition is 10logP(t), 10logP(t-T),...
is obtained as a 10-bit digital signal. This quantization circuit 33 output signal is supplied to a delay circuit 34 that delays radar transmission repetition time T and a subtraction circuit 35, so that the subtraction circuit 35 output signal becomes {10logP(t)−10logP(t−T)}. Become.

この減算回路35出力信号は変換回路36に供
給され、前記{10logP(t)−10log(t−T)}に対
応した対数変換出力信号10log〔1−10−{10logP
(t)−10logP(t−T)}/10〕を導出する。
This subtraction circuit 35 output signal is supplied to a conversion circuit 36, which converts the logarithmic conversion output signal 10log[1-10-{10logP] corresponding to {10logP(t)-10log(t-T)}
(t)-10logP(t-T)}/10].

この変換回路36は例えば中央演算処理装置
(CPU)により入力信号ごとに対数演算するよう
構成してもよく、あるいはあらかじめ入力信号値
に対応した出力信号値を算出しテーブル化してお
いて、リードオンリメモリ(ROM)等の構成に
より入力信号値に対応した出力信号値を読み出し
供給するように構成してもよい。このようにして
変換回路36出力信号と前記量子化回路33から
の出力信号とを出力回路37に供給し、この両信
号を加算回路371で加算演算する。
This conversion circuit 36 may be configured such that a central processing unit (CPU) performs a logarithmic operation for each input signal, or the conversion circuit 36 may be configured such that a central processing unit (CPU) performs a logarithmic operation for each input signal, or the output signal value corresponding to the input signal value is calculated and tabulated in advance, and the conversion circuit 36 is read-only. The configuration may be such that a memory (ROM) or the like is configured to read and supply an output signal value corresponding to an input signal value. In this way, the output signal of the conversion circuit 36 and the output signal from the quantization circuit 33 are supplied to the output circuit 37, and the addition circuit 371 performs an addition operation on these two signals.

一方、前記減算回路35出力信号は検知回路3
8にも供給され、振幅比較回路382で閾値発生
回路381により発生した閾値信号と比較され
る。そこで振幅比較回路382出力信号はゲート
回路372に供給され、前記減算回路35出力信
号が前記閾値信号より大きい時にのみ加算回路3
71出力信号を出力するようにゲート回路372
を制御する。
On the other hand, the output signal of the subtraction circuit 35 is
8, and is compared with the threshold signal generated by the threshold generation circuit 381 in the amplitude comparison circuit 382. Therefore, the output signal of the amplitude comparison circuit 382 is supplied to the gate circuit 372, and only when the output signal of the subtraction circuit 35 is greater than the threshold signal, the addition circuit 3
Gate circuit 372 to output the 71 output signal
control.

第4図は本発明による装置の信号波形を示すも
ので、波形aは対数特性受信回路32出力信号波
形、波形bは加算回路371出力信号波形であ
る。この信号波形bは第2図波形bに示すものと
同じであり、加算回路371出力段では変動成分
が重畳したグランドクラツタ41が大きな変動成
分44として検出される。しかし、減算回路35
出力段は第4図に示す波形Cのように変動成分が
重畳したグランドクラツタ45は小さい。この減
算回路35出力を検知回路38に加える。この検
知回路38は最小気象情報量検知レベル(第4図
波形Cにおける46)を発生する閾値発生回路3
81や、この閾値発生回路381出力信号と減算
回路35出力信号との振幅を比較する振幅比較回
路382から構成されており、前記減算回路35
出力レベルが前記最小気象情報量検知レベルを越
えた時に、前記振幅比較回路382から出力信号
を導出する。この出力信号は例えば第4図波形d
で示される。そしてこの出力信号を加算回路37
1出力段に設けたゲート回路372にゲート信号
として供給することによりこのゲート回路372
からは第4図の波形eのような出力信号、即ち、
雑音成分43を含まない気象情報、例えば雨を表
わす信号42を抽出することができる。
FIG. 4 shows signal waveforms of the device according to the present invention, in which waveform a is the output signal waveform of the logarithmic characteristic receiving circuit 32, and waveform b is the output signal waveform of the adder circuit 371. This signal waveform b is the same as that shown in waveform b in FIG. 2, and the ground clutter 41 on which the fluctuation components are superimposed is detected as a large fluctuation component 44 at the output stage of the adder circuit 371. However, the subtraction circuit 35
In the output stage, the ground clutter 45 in which fluctuating components are superimposed as shown in waveform C shown in FIG. 4 is small. The output of this subtraction circuit 35 is applied to a detection circuit 38. This detection circuit 38 is a threshold generation circuit 3 that generates the minimum meteorological information amount detection level (46 in waveform C in FIG. 4).
81 and an amplitude comparison circuit 382 that compares the amplitude of the output signal of the threshold value generation circuit 381 and the output signal of the subtraction circuit 35.
When the output level exceeds the minimum weather information amount detection level, an output signal is derived from the amplitude comparison circuit 382. This output signal is, for example, the waveform d in Figure 4.
It is indicated by. Then, this output signal is added to the adder circuit 37.
This gate circuit 372 is supplied as a gate signal to the gate circuit 372 provided in the first output stage.
, an output signal like the waveform e in FIG. 4, i.e.,
Weather information that does not include noise components 43, for example, a signal 42 representing rain, can be extracted.

このように本発明装置では従来のレーダ信号処
理装置のMTI方式における気象情報の定量的測
定能力を劣化させず、しかもグランドクラツタ等
の不要情報を効果的に除去して正確な気象情報測
定のできる利点がある。なお、第3図において、
ゲート回路372を加算回路371の出力段に付
加しているが、これを加算回路371の入力段に
付加することによつても同様な効果を得ることが
できる。
In this way, the device of the present invention does not degrade the quantitative measurement ability of weather information in the MTI method of conventional radar signal processing devices, and moreover effectively removes unnecessary information such as ground clutter, thereby making it possible to accurately measure weather information. There are advantages that can be achieved. In addition, in Figure 3,
Although the gate circuit 372 is added to the output stage of the adder circuit 371, the same effect can be obtained by adding it to the input stage of the adder circuit 371.

又、第3図の一実施例では遅延回路34、減算
回路35、変換回路36および出力回路37によ
つて構成される単一消去フイルタを用いた例で説
明したが、この単一消去フイルタに更に1回路付
加したいわゆるダブル消去フイルタの場合におい
ても本発明が適用できることは勿論である。
Furthermore, in the embodiment shown in FIG. 3, a single erasure filter composed of a delay circuit 34, a subtraction circuit 35, a conversion circuit 36, and an output circuit 37 is used. It goes without saying that the present invention can also be applied to a so-called double erasure filter in which one additional circuit is added.

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

第1図は従来のレーダ信号処理装置を示す構成
図、第2図は第1図に示した装置の動作を説明す
るための信号波形図、第3図は本発明によるレー
ダ信号処理装置の一実施例を示す構成図、第4図
は第3図に示した装置の動作を説明するための信
号波形図である。 31…空中線、32…対数特性受信回路、33
…量子化回路、34…遅延回路、35…減算回
路、36…変換回路、37…出力回路、38…検
知回路。
FIG. 1 is a configuration diagram showing a conventional radar signal processing device, FIG. 2 is a signal waveform diagram for explaining the operation of the device shown in FIG. 1, and FIG. 3 is a diagram of a radar signal processing device according to the present invention. FIG. 4 is a block diagram showing the embodiment, and is a signal waveform diagram for explaining the operation of the apparatus shown in FIG. 3. 31... Antenna, 32... Logarithmic characteristic receiving circuit, 33
...Quantization circuit, 34...Delay circuit, 35...Subtraction circuit, 36...Conversion circuit, 37...Output circuit, 38...Detection circuit.

Claims (1)

【特許請求の範囲】[Claims] 1 空中線で捕捉された目標反射レーダ信号P
(t)を導入しAlogKP(t)に対応した信号(Aは定
数)を出力する対数特性受信回路と、この受信回
路の出力信号を振幅方向に量子化する量子化回路
と、この量子化回路の出力信号をレーダ送信繰返
し時間だけ遅延する遅延回路と、この遅延回路の
出力信号を前記量子化回路の出力信号から減算し
信号S(t)を導出する減算回路と、この減算回路
の出力信号が供給されAlogK{1−K-S(t)/A}に対
応した信号を導出する変換回路と、前記減算回路
の出力信号が供給され予じめ決められた所定レベ
ルより大きい信号を検出する検出手段と、この検
出手段の検出出力がある場合にのみ前記変換回路
の出力信号と前記量子化回路の出力信号との加算
信号を出力する出力手段とを具備するレーダ信号
処理装置。
1 Target reflected radar signal P captured by antenna
(t) and outputs a signal corresponding to Alog K P(t) (A is a constant); a quantization circuit that quantizes the output signal of this reception circuit in the amplitude direction; a delay circuit that delays the output signal of the quantization circuit by a radar transmission repetition time; a subtraction circuit that subtracts the output signal of the delay circuit from the output signal of the quantization circuit to derive a signal S(t); a conversion circuit that is supplied with an output signal and derives a signal corresponding to Alog K {1-K -S(t)/A }; and a signal that is supplied with an output signal of the subtraction circuit and that is higher than a predetermined level. A radar signal processing device comprising: a detection means for detecting; and an output means for outputting a sum signal of the output signal of the conversion circuit and the output signal of the quantization circuit only when there is a detection output of the detection means.
JP697480A 1980-01-25 1980-01-25 Radar signal processor Granted JPS56104265A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP697480A JPS56104265A (en) 1980-01-25 1980-01-25 Radar signal processor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP697480A JPS56104265A (en) 1980-01-25 1980-01-25 Radar signal processor

Publications (2)

Publication Number Publication Date
JPS56104265A JPS56104265A (en) 1981-08-19
JPS636835B2 true JPS636835B2 (en) 1988-02-12

Family

ID=11653163

Family Applications (1)

Application Number Title Priority Date Filing Date
JP697480A Granted JPS56104265A (en) 1980-01-25 1980-01-25 Radar signal processor

Country Status (1)

Country Link
JP (1) JPS56104265A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4533915A (en) * 1982-02-16 1985-08-06 Sperry Corporation Radar terrain signal suppressor
US4628318A (en) * 1983-12-02 1986-12-09 Rockwell International Corporation Ground clutter suppression technique

Also Published As

Publication number Publication date
JPS56104265A (en) 1981-08-19

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