JPS6361982A - Synthetic aperture radar - Google Patents

Synthetic aperture radar

Info

Publication number
JPS6361982A
JPS6361982A JP20602286A JP20602286A JPS6361982A JP S6361982 A JPS6361982 A JP S6361982A JP 20602286 A JP20602286 A JP 20602286A JP 20602286 A JP20602286 A JP 20602286A JP S6361982 A JPS6361982 A JP S6361982A
Authority
JP
Japan
Prior art keywords
wave
stc
received
timing
received wave
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.)
Granted
Application number
JP20602286A
Other languages
Japanese (ja)
Other versions
JPH055313B2 (en
Inventor
Kyoko Miyashita
京子 宮下
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.)
National Institute of Advanced Industrial Science and Technology AIST
Original Assignee
Agency of Industrial Science and Technology
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 Agency of Industrial Science and Technology filed Critical Agency of Industrial Science and Technology
Priority to JP20602286A priority Critical patent/JPS6361982A/en
Publication of JPS6361982A publication Critical patent/JPS6361982A/en
Publication of JPH055313B2 publication Critical patent/JPH055313B2/ja
Granted legal-status Critical Current

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  • Radar Systems Or Details Thereof (AREA)

Abstract

PURPOSE:To automatically perform accurate sensitive time control(STC) over a received time automatically and applying it as control timing. CONSTITUTION:A transmission part 1 modulates and amplifies a pulse signal to generate a sent wave and a transmission/reception branching filter part 2 separates a sent wave and a received wave; and the sent wave is transmitted to the ground from a transmitting and receiving antenna 3 and its reflected wave from the ground is received. A reception part 3 demodulates the received wave to detect the pulse signal. Then an STC automatic control part 11 has a function 12 for detecting the reception start timing of the received wave on then basis of the transmission timing of the sent wave as a start point and a function 13 for setting the STC start timing of the received wave automatically by using the detected timing. The STC automatic control part 11 uses a comparator and a counter to measure the actual delay from the sent wave to the received wave and controls the STC start timing with the value.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 コントロール(Senaitiv Time Cont
rol :以下STCとする)の開始タイミングを自動
制御する衛星搭載用合成開口レーダに関するものである
[Detailed description of the invention] [Industrial application field] Control
This invention relates to a satellite-mounted synthetic aperture radar that automatically controls the start timing of STC (hereinafter referred to as STC).

〔従来の技術〕[Conventional technology]

第3図は従来の受信機のSTC開始タイミングの制御方
式を用いた合成開口レーダの機能図で、(1)はパルス
信号を変調増幅して送信波を発生するための送信部、(
2)は送信波と受信波を分離するための送受分波部、(
3)は送受信用アンテナ、(4)は受信波を復調し、パ
ルス信号を検波するための受信部。
Fig. 3 is a functional diagram of a synthetic aperture radar using a conventional receiver STC start timing control system, in which (1) shows a transmitter for modulating and amplifying a pulse signal to generate a transmission wave;
2) is a transmitting/receiving demultiplexing section for separating the transmitted wave and the received wave, (
3) is a transmitting and receiving antenna, and (4) is a receiving section for demodulating received waves and detecting pulse signals.

(5)は地上にてSTC開始タイミングを計算によって
求め、その値をコマンドとして衛星搭載合成開口レーダ
に送信するための地上局、(6)はそのコマンドを受信
する受信部、(7)は(6)によって受信されたコマン
ドにより得られたSTC開始タイミングを適用し受信波
のSTC制御を行うSTC制御部である。
(5) is a ground station that calculates the STC start timing on the ground and sends that value as a command to the satellite-mounted synthetic aperture radar; (6) is a receiver that receives the command; (7) is ( 6) is an STC control unit that performs STC control of received waves by applying the STC start timing obtained by the command received in step 6).

次に動作について説明する。第4図は、従来の方式をタ
イミングチャートに表わしたものであり。
Next, the operation will be explained. FIG. 4 shows a timing chart of the conventional system.

(8)は送信波、(9)は地上から反射された受信波、
aユ地上からコマンドで与えられる送信波から受信波ま
での遅れ時間つまりSTC開始時間であり、この値を用
いて、制御開始のタイミングがとられていた。このよう
に、従来は地上において衛星の軌道・姿勢条件等をとり
込んで、あらかじめ計算された遅れ時間をコマンドによ
り衛星へ送り2合成開口レーダにおいて、その値を用い
、受信波のSTCO開始タイミングを制御していた。
(8) is the transmitted wave, (9) is the received wave reflected from the ground,
This is the delay time from the transmitted wave to the received wave given by a command from the ground, that is, the STC start time, and this value was used to determine the timing for starting control. In this way, conventionally, the orbit and attitude conditions of the satellite are taken in on the ground, and the pre-calculated delay time is sent to the satellite using a command.The second synthetic aperture radar uses this value to determine the STCO start timing of the received wave. I was in control.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

従来の合成開口レーダは受信波STC制御方式として以
上のような方式を用いているので、地上において送信波
から受信波までの遅れ時間をあらかじめ計算しなければ
ならず、そのためには搭載されている衛星の軌道条件及
び姿勢条件等を厳密に解析することが必要で、またそれ
らは計算による値であるため、実際の遅れ時間に対して
多少正確さに欠ける゛等の問題点があった。
Conventional synthetic aperture radar uses the above-mentioned method for controlling the received wave STC, so the delay time from the transmitted wave to the received wave must be calculated in advance on the ground. It is necessary to strictly analyze the orbital conditions and attitude conditions of the satellite, and since these are calculated values, there are problems such as a lack of accuracy to the actual delay time.

この発明は上記のような問題点を解消するためになされ
たもので、従来、地上で計算しなければならなかった遅
れ時間、つまりSTC開始時間は。
This invention was made to solve the above-mentioned problems. Conventionally, the delay time, that is, the STC start time, had to be calculated on the ground.

合成開口レーダ内で自動的に求めることができるととも
に、その値が、実際の生データであるため受信波とST
C制御のタイミングを確実に合せることができるSTC
自動制御が実現できる合成開口レーダを得ることを目的
とする。
It can be automatically determined within the synthetic aperture radar, and since the value is actual raw data, it can be used to compare received waves and ST.
STC that can reliably match the timing of C control
The purpose of this study is to obtain a synthetic aperture radar that can be automatically controlled.

〔問題点を解決するための手段〕[Means for solving problems]

この発明に係る合成開口レーダは、衛星搭載用合成開口
レーダの受信波をSTC制御する際制御開始時間、つま
り送信パルスから受信波までの遅れ時間を合成開口レー
ダ内で自動的にカウントし。
The synthetic aperture radar according to the present invention automatically counts the control start time, that is, the delay time from the transmitted pulse to the received wave, within the synthetic aperture radar when performing STC control on the received waves of the satellite-mounted synthetic aperture radar.

それによりSTCの開始タイミングの自動化をはかった
ものである。
This aims to automate the STC start timing.

〔作 用〕[For production]

この発明における合成開口レーダは、受信波のSTOに
おいて、自動的に実際の制御開始遅れ時間を求め、それ
を制御開始タイミングとして適用することにより、従来
の方式に比べて、非常に容易となるとともに、制御開始
“タイミングと受信波の受信タイミングとのタイミング
合せがより正確に行われる。
The synthetic aperture radar according to the present invention automatically determines the actual control start delay time in the STO of the received wave and applies it as the control start timing, making it much easier than conventional methods. , the control start timing and the reception timing of the received wave can be more accurately aligned.

〔実施例〕〔Example〕

以下、この発明の一実施例を図について説明する。第1
図において、(1)〜(4)は従来と同じものである。
An embodiment of the present invention will be described below with reference to the drawings. 1st
In the figure, (1) to (4) are the same as the conventional one.

Uは3TC自動制御部であって、この制御部αυは送信
波の送信タイミングを起点として受信波の受信開始タイ
ミングを検出する機能α力と、検出されたタイミングを
用いて受信波のSTC開始タイミングを自動設定する機
能(I■とを備えている。
U is a 3TC automatic control unit, and this control unit αυ has a function α which detects the reception start timing of the reception wave using the transmission timing of the transmission wave as a starting point, and uses the detected timing to determine the STC start timing of the reception wave. Equipped with a function to automatically set (I).

STC自動制御部では、コンパレータ及びカウンタを用
いて、送信波から受信波までの実際の遅れ時間を測定し
、その値によってSTC開始タイミングの制御を行う。
The STC automatic control unit uses a comparator and a counter to measure the actual delay time from the transmitted wave to the received wave, and controls the STC start timing based on the measured value.

まず、受信波の電圧振幅レベルに、受信波が受信された
ことの判断基塾として、ある電圧振幅レベルをスレッシ
ュホールドレベルとして設定スル。
First, a certain voltage amplitude level is set as a threshold level for the voltage amplitude level of the received wave as a basis for determining that the received wave has been received.

次に送信波の出力タイミングに合わせ、コンパレータに
よって受信波の有無の検出を開始し、同時にカウンタを
動作し始める。その後、コンパレータが受信波のスレッ
シュホールドレベルとして設定したあるレベル以上の受
信レベルを検出するまで、カウンタは動作し続け、コン
パレータの受信波検出と同時に、停止するようになって
いる。
Next, in accordance with the output timing of the transmitted wave, the comparator starts detecting the presence or absence of the received wave, and at the same time starts operating the counter. Thereafter, the counter continues to operate until the comparator detects a reception level equal to or higher than a certain level set as the threshold level of the reception wave, and stops at the same time as the comparator detects the reception wave.

このよりに、 STC自動制御部Uにおいて、送信波か
ら受信波までの遅れ時間を正確に検出し、そのタイミン
グを用いてSTC制御のためのSTCゲート信号を発生
させ、自動的に受信波のSTC制御を行うことができる
As a result, the STC automatic control unit U accurately detects the delay time from the transmitted wave to the received wave, uses that timing to generate an STC gate signal for STC control, and automatically adjusts the STC of the received wave. can be controlled.

第2図は、この発明による方式を用いた場合のタイミン
グチャートを表わしたものであり、(1)は従来と同じ
ものである。α4はあるスレッシュホールドレベルが設
定された受信波を示し、霞は受信波に対して設定された
あるスレッシュホールドレベルを示し、α0はSTC自
動制御方式によりSTC開始タイミングが制御されたS
TC制御のゲート信号であり、ここでT2がSTC自動
制御部の中で。
FIG. 2 shows a timing chart when the method according to the present invention is used, and (1) is the same as the conventional one. α4 indicates a received wave with a certain threshold level set, haze indicates a certain threshold level set for the received wave, and α0 indicates STC start timing controlled by the STC automatic control method.
This is the gate signal for TC control, where T2 is in the STC automatic control section.

コンパレータを用い受信波の有無を判定し、それにとも
ない受信波の遅れ時間をカウントすることにより求めら
れたSTC開始時間である。この値を用いて制御開始の
タイミングが正確にとられている。
This is the STC start time determined by determining the presence or absence of a received wave using a comparator and counting the delay time of the received wave accordingly. This value is used to accurately determine the timing for starting control.

〔発明の効果〕〔Effect of the invention〕

以上のように、この発明によれば衛星搭載用合成開口レ
ーダにおいて、受信波のSTC開始タイミングを自動的
に制御できるような方式を用いたので、地上での計算及
びコマンド送出を行わずに済み、またハード的に実際に
求められた値を用いての制御であるため精度の高い制御
が容易に行えるという効果がある。
As described above, according to the present invention, in the satellite-mounted synthetic aperture radar, a method is used that can automatically control the STC start timing of the received wave, so there is no need to perform calculations or send commands on the ground. Furthermore, since the control is performed using values actually obtained using hardware, there is an effect that highly accurate control can be performed easily.

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

第1図はこの発明の一実施例による機能図、第2図はこ
の発明のSTC自動制御方式を用いた動作状況を示すタ
イミングチャート、第3図は従来の方式による機能図、
第4図は従来の方式を用いた動作状況を示すタイミング
チャートである。 図において、(1)は送信部、(2)は送受分波部、(
3)は送受信用アンテナ、(4)は受信部、(5)は地
上局。 (6)はコマンド受信部、(7)はSTC制御部、(8
)は送信波、(9)は受信波、α1はSTCゲート信号
、11)はSTC自動制御部、■はSTC自動制御部に
備えられている受信波の受信タイミングを検出する機能
、α罎は8TC自動制御部に備えられている。受信波の
STC開始タイミングを自動設定する機能、α尋はある
スレッシュホールドレベルが設定された受信波、α9は
受信波に設定されたあるスレッシュホールドレベル、α
0はSTC自動制御部によってタイミングを制御された
STCゲート信号である。 なお図中、同一符号は同一、又は相当部分を示す。 特許出衰人工業技術院長 S4灸卑ニ @1図 +r:src自動利uF=Il! 第 2 図 求のうjllろSTC開始的聞 第3rA 第4図
FIG. 1 is a functional diagram according to an embodiment of the present invention, FIG. 2 is a timing chart showing an operating situation using the STC automatic control method of the present invention, and FIG. 3 is a functional diagram according to a conventional method.
FIG. 4 is a timing chart showing the operating situation using the conventional method. In the figure, (1) is a transmitting section, (2) is a transmitting/receiving demultiplexing section, (
3) is a transmitting and receiving antenna, (4) is a receiving section, and (5) is a ground station. (6) is a command receiving section, (7) is an STC control section, (8
) is the transmitted wave, (9) is the received wave, α1 is the STC gate signal, 11) is the STC automatic control unit, ■ is the function of detecting the reception timing of the received wave provided in the STC automatic control unit, α is It is provided in the 8TC automatic control section. A function that automatically sets the STC start timing of the received wave, α9 is the received wave with a certain threshold level set, α9 is the certain threshold level set for the received wave, α
0 is an STC gate signal whose timing is controlled by the STC automatic control section. In the figures, the same reference numerals indicate the same or equivalent parts. Patent Output Industrial Technology Director S4 Moxibustion Bi @ 1 Figure + r: src automatic benefit uF = Il! 2nd figure 3rA Figure 4

Claims (1)

【特許請求の範囲】[Claims] パルス信号を変調増幅して送信波を発生するための送信
部と、送信波と受信波を分離するための送受分波部と、
送信波を地上へ送信し、地上からの反射波を受信するた
めの送受信用アンテナと、受信波を復調しパルス信号を
検波するための受信部と、送信波の送信タイミングを起
点として受信波の受信開始タイミングを検出する機能及
び前記のタイミングの検出により受信波のセンシテイブ
・タイム・コントロール(Sensitiv Time
 Control)の開始タイミングを自動設定する機
能を備えたセンシテイブ・タイム・コントロール自動制
御部とで構成したことを特徴とする衛星搭載用合成開口
レーダ。
a transmitting section for modulating and amplifying the pulse signal to generate a transmitting wave; a transmitting/receiving demultiplexing section for separating the transmitting wave and the receiving wave;
A transmitting/receiving antenna that transmits the transmitted wave to the ground and receives the reflected wave from the ground, a receiving section that demodulates the received wave and detects the pulse signal, and a receiver that demodulates the received wave and detects the pulse signal. Sensitive time control of received waves is achieved by the function of detecting the reception start timing and the detection of the above-mentioned timing.
What is claimed is: 1. A synthetic aperture radar for use on a satellite, comprising a sensitive time control automatic control unit having a function of automatically setting the start timing of the control.
JP20602286A 1986-09-03 1986-09-03 Synthetic aperture radar Granted JPS6361982A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20602286A JPS6361982A (en) 1986-09-03 1986-09-03 Synthetic aperture radar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20602286A JPS6361982A (en) 1986-09-03 1986-09-03 Synthetic aperture radar

Publications (2)

Publication Number Publication Date
JPS6361982A true JPS6361982A (en) 1988-03-18
JPH055313B2 JPH055313B2 (en) 1993-01-22

Family

ID=16516603

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20602286A Granted JPS6361982A (en) 1986-09-03 1986-09-03 Synthetic aperture radar

Country Status (1)

Country Link
JP (1) JPS6361982A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03130683A (en) * 1989-10-17 1991-06-04 Nec Corp Synthetic aperture radar apparatus

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59182379A (en) * 1983-03-31 1984-10-17 Mitsubishi Electric Corp Synthetic aperture radar
JPS6088378A (en) * 1983-10-20 1985-05-18 Nec Corp Radar equipment
JPS617485A (en) * 1984-06-21 1986-01-14 Nec Corp Radar apparatus

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59182379A (en) * 1983-03-31 1984-10-17 Mitsubishi Electric Corp Synthetic aperture radar
JPS6088378A (en) * 1983-10-20 1985-05-18 Nec Corp Radar equipment
JPS617485A (en) * 1984-06-21 1986-01-14 Nec Corp Radar apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03130683A (en) * 1989-10-17 1991-06-04 Nec Corp Synthetic aperture radar apparatus

Also Published As

Publication number Publication date
JPH055313B2 (en) 1993-01-22

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