JPS59184875A - Synthetic aperature radar - Google Patents

Synthetic aperature radar

Info

Publication number
JPS59184875A
JPS59184875A JP58059552A JP5955283A JPS59184875A JP S59184875 A JPS59184875 A JP S59184875A JP 58059552 A JP58059552 A JP 58059552A JP 5955283 A JP5955283 A JP 5955283A JP S59184875 A JPS59184875 A JP S59184875A
Authority
JP
Japan
Prior art keywords
antenna beam
coverage
pulse
received
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.)
Pending
Application number
JP58059552A
Other languages
Japanese (ja)
Inventor
Makoto Ono
誠 小野
Hirokazu Tanaka
宏和 田中
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP58059552A priority Critical patent/JPS59184875A/en
Publication of JPS59184875A publication Critical patent/JPS59184875A/en
Pending legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO 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
    • G01S13/00—Systems 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
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/89—Radar or analogous systems specially adapted for specific applications for mapping or imaging
    • G01S13/90—Radar or analogous systems specially adapted for specific applications for mapping or imaging using synthetic aperture techniques, e.g. synthetic aperture radar [SAR] techniques

Landscapes

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

Abstract

PURPOSE:To widen an observation area without increasing the transmitting power by controlling the transmission phase of a phase shifter, and controlling the direction of an antenna beam. CONSTITUTION:The high frequency pulse power of a transmitter 2 is fed to antennas 1-1, 1-2 through a transmission and reception branching filter 3, a power distributor 5 and a phase shifter 6, and radiated to space. Also, when an excitation phase is controlled by the phase shifter 6 so that an antenna beam is directed to the direction of a coverage A at the time when a transmitting pulse 7-1 is radiated, and the antenna beam is directed to the direction of a coverage B at the time when a transmitting pulse 7-2 is radiated, and a phase of the phase shifter 6 is controlled so that the antenna beam is directed to the direction of the coverage A at the time when a reflected echo 8-1 is received, and the antenna beam is directed to the direction of the coverage B at the time when a reflected echo 8-2 is received, each reflected echo, and the transmitting pulse and the received echo are not overlapped, and the coverage A and B are covered with the whole.

Description

【発明の詳細な説明】 この発明は人工衛星に搭載する合成開口レーダに関する
ものである。合成開口レーダは昼夜天候に関係なく極め
て高い距離分解能の映像が得られるリモートセンサであ
る。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a synthetic aperture radar mounted on an artificial satellite. Synthetic aperture radar is a remote sensor that can provide images with extremely high distance resolution regardless of day or night weather.

第1図は従来の合成開口レーダの動作原理を示す図であ
る。レーダ送@機(2)により発生した高周波パルス電
波は、送受分波器(3)及びアンテナ(1)を柱て観ひ
j方向に放射される。観測域からの反射波は再びアンテ
ナ(1)で受信され、送受分波器(3)を経て、受信機
(4)で受信される。この受信信号を信号処理する事に
より高分解能画像を得るものである。
FIG. 1 is a diagram showing the operating principle of a conventional synthetic aperture radar. High-frequency pulse radio waves generated by the radar transmitter (2) are radiated in the J direction through the transmitter/receiver duplexer (3) and the antenna (1). The reflected wave from the observation area is received again by the antenna (1), passes through the transmitter/receiver splitter (3), and is received by the receiver (4). A high-resolution image is obtained by processing this received signal.

レーダは大電力のパルス電波を放射するのでパルス送信
中は受信機は動作させる事が出来ない。従って、送信パ
ルスの繰返し周波数fUレーダからみた観測域の最近点
までの距離をRI  p最遠点までの距離をR3とする
とき9次のような条件を商すように選択される。
Since radar emits high-power pulse radio waves, the receiver cannot operate while the pulse is being transmitted. Therefore, the repetition frequency of the transmitted pulse fU is selected so as to satisfy the following conditions when the distance to the nearest point of the observation area as seen from the radar is RI p and the distance to the farthest point is R3.

こ\にCは光速、nは正の整数である。Here, C is the speed of light and n is a positive integer.

以上のように、パルス繰返し周波数を選定すると、定性
的に送信パルスと受信エコーのタイミングは第2図に示
すようになって、送信時間間隔Ttよυ、受イ1時間幅
’rrか短くなる。一方、観測に際しては、観測域が出
来る限り広い事が望1れるが、送信時間間隔と受1′呂
時間幅を一致させるようにすると、アンテナビームの覆
域を広げる事になり、利得が吐下する。合成−ロレーダ
のl[!!I像の信号対雑音比は送信電力とアンテナ利
得の2乗の槓に比例するので、観測幅を広くすると回じ
イぎ号対雑音比を得るために観測幅の2乗に比例して送
信電力を増加する必要がある。この発明は、従来のレー
ダの持つこのような問題点を除去するためになされたも
ので、送信電力を増加せずに観測域を広くする手段を提
供するものである。以下2図面によυこの発明の内容を
詳細に説明する。
As described above, when the pulse repetition frequency is selected, qualitatively the timing of the transmitted pulse and the received echo becomes as shown in Fig. 2, and the transmission time interval Tt υ and the receiving time width 'rr become shorter. . On the other hand, during observation, it is desirable for the observation area to be as wide as possible, but if the transmission time interval and reception time interval are made to match, the coverage area of the antenna beam will be expanded and the gain will be reduced. down. Synthesis - Loreda's l[! ! The signal-to-noise ratio of the I-image is proportional to the square of the transmission power and the antenna gain, so if the observation width is widened, the signal-to-noise ratio of the I-image is proportional to the square of the observation width. Need to increase power. This invention was made to eliminate such problems with conventional radars, and provides a means for widening the observation area without increasing transmission power. The contents of this invention will be explained in detail with reference to the following two drawings.

第3図(ばこの発明の一実施例になる合成開口レーダの
構成を説明するための図である。図において、(1)は
2個以上の素子からなる1次元フェーズドアレーアンテ
ナ、(2)は送信機、(3)は送受分波器。
FIG. 3 (This is a diagram for explaining the configuration of a synthetic aperture radar which is an embodiment of the present invention. In the figure, (1) is a one-dimensional phased array antenna consisting of two or more elements, (2) is a transmitter, and (3) is a transmitter/receiver duplexer.

(4)は受信機、(5)は電力分配器、(6)は移相器
である。
(4) is a receiver, (5) is a power divider, and (6) is a phase shifter.

贅た。(A)およびCB) Uアンテナビームの覆域で
ある。
Luxurious. (A) and CB) Coverage of U antenna beam.

甘だ、第4図はパルスタイミングを示す図であって、(
7)は2個の連続したパルス列、(8)はそれぞれのパ
ルスに対応する受信エコーを表わす。
That's naive. Figure 4 is a diagram showing the pulse timing, and (
7) represents two consecutive pulse trains, and (8) represents the received echo corresponding to each pulse.

以上の図において、送信機(2)より発生した^周波パ
ルス電力は、送受分波器(3)、電力分配器(5)。
In the above figure, the ^-frequency pulse power generated from the transmitter (2) is sent to the transmitter/receiver splitter (3) and the power divider (5).

及び移相器(6)を経由してアンテナ(+−1)及び(
1−2)に給電され、空間に放射される。移相器の透過
位相を制御してやればアンテナビームの方向は観測域(
A)または観測域(BJ化覆うようにそのビーム方向が
変化する。観測域からの反射波は逆の道をたどって送受
分波器(3)を経由し受信機(4)で受信される。
and the antenna (+-1) and (
1-2) and radiates into space. By controlling the transmission phase of the phase shifter, the direction of the antenna beam can be adjusted to the observation range (
A) or the observation area (BJ) The beam direction changes to cover the observation area.The reflected wave from the observation area follows the opposite path and is received by the receiver (4) via the transmitter/receiver splitter (3). .

第4図において、送信パルス(,7−1)が放射される
時刻にアンテナビームが覆域(、A)の方向を向き、(
7−2)が放射される時刻にアンテナビームが覆域(B
)の方向を向くように移相器(6)により励振位相が制
御され1反射エコー(8−1)を受信する時刻にアンテ
ナビームが覆域(A)の方向を向き反射−cコ−(8−
2)を受信する時刻にアンテナビームが覆域(B)の方
向を向くように移相器(6)の位相が制御されていれば
、互の反射エコー同志も。
In Fig. 4, at the time when the transmission pulse (, 7-1) is emitted, the antenna beam is directed to the coverage area (, A), and (
7-2) is emitted when the antenna beam reaches the coverage area (B
), the excitation phase is controlled by the phase shifter (6), and at the time when one reflected echo (8-1) is received, the antenna beam faces the direction of the coverage area (A) and the reflected echo (c) ( 8-
2) If the phase of the phase shifter (6) is controlled so that the antenna beam points in the direction of the coverage area (B) at the time of receiving the signal, the mutual reflected echoes will also be the same.

また送信パルスと受信エコーも重なることなく受信され
、全体で覆域(A)と覆域(B)を覆う事が出来る。
Further, the transmitted pulse and the received echo are received without overlapping, and the coverage area (A) and the coverage area (B) can be covered as a whole.

さらに、全体の覆域を同時に覆うようにビーム幅の広い
アンテナを用いる場合に比べ、アンテナビームの覆域が
半分になるため、アンテナ利得は倍になp、送信パルス
(7−1)及び(7−2)の電力は4分の1で良い。
Furthermore, compared to the case where an antenna with a wide beam width is used to simultaneously cover the entire coverage area, the coverage area of the antenna beam is halved, so the antenna gain is doubled, p, and the transmission pulse (7-1) and ( 7-2) requires only one-fourth the power.

従って、2個のパルスを連続して放射しても。Therefore, even if two pulses are emitted in succession.

全電力は半分で済む事になる。The total power consumption will be halved.

以上のようにこの発明によれば、広い覆域のデータを少
い電力の送信機で得る事が出来、衛星搭載用としてその
効果は極めて太きい。
As described above, according to the present invention, data covering a wide area can be obtained using a transmitter with low power consumption, and the effect is extremely large when used on a satellite.

なお、この発明は以上の実施例に限られる事なく1例え
ば2台の送信機を用いて2個のアンテナを別々に励振す
るようにしても全く同様に実施出来る。
Note that the present invention is not limited to the above-described embodiments, and can be implemented in exactly the same way by using one, for example, two transmitters to separately excite two antennas.

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

第1図は従来の合成開口レーダの説明図、第2図は従来
のレーダにおけるノ(ルスタイミングを示す図、第3図
はこの発明の説明図、第4図はこの発明のパルスタイミ
ングを示す図である。図において、(1)はアンテナ、
(2)は送信機、(4)は受信機。 (61は移相器、(7)は送信ノ(ルス、(8)は受信
エコーである。なお図中、同一あるいは相当する部分は
同一符号を付しである。 代理人大岩増雄
Fig. 1 is an explanatory diagram of a conventional synthetic aperture radar, Fig. 2 is a diagram showing the pulse timing in the conventional radar, Fig. 3 is an explanatory diagram of the present invention, and Fig. 4 is a diagram showing the pulse timing of the present invention. In the figure, (1) is an antenna;
(2) is a transmitter, and (4) is a receiver. (61 is the phase shifter, (7) is the transmitting noise, and (8) is the receiving echo. In the figure, the same or corresponding parts are given the same reference numerals. Agent Masuo Oiwa

Claims (1)

【特許請求の範囲】 送信パルスが2個以上続いて放射される手段と。 1面内でビームを走査する1次元フエイズドアレーアン
テナと2反射電波を受信する手段とを備えて構成したこ
とを特徴とする合成開口レーダ。
[Claims:] Means for emitting two or more transmission pulses in succession. A synthetic aperture radar comprising a one-dimensional phased array antenna that scans a beam in one plane and means for receiving two reflected radio waves.
JP58059552A 1983-04-05 1983-04-05 Synthetic aperature radar Pending JPS59184875A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58059552A JPS59184875A (en) 1983-04-05 1983-04-05 Synthetic aperature radar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58059552A JPS59184875A (en) 1983-04-05 1983-04-05 Synthetic aperature radar

Publications (1)

Publication Number Publication Date
JPS59184875A true JPS59184875A (en) 1984-10-20

Family

ID=13116525

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58059552A Pending JPS59184875A (en) 1983-04-05 1983-04-05 Synthetic aperature radar

Country Status (1)

Country Link
JP (1) JPS59184875A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03239982A (en) * 1990-02-19 1991-10-25 Nec Corp Synthetic aperture radar equipment

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57139677A (en) * 1981-02-23 1982-08-28 Toshiba Corp Composite-opening plane type radar device

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57139677A (en) * 1981-02-23 1982-08-28 Toshiba Corp Composite-opening plane type radar device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03239982A (en) * 1990-02-19 1991-10-25 Nec Corp Synthetic aperture radar equipment

Similar Documents

Publication Publication Date Title
US5059966A (en) Synthetic aperture radar system
EP0520666B1 (en) Ultra wideband radar employing synthesized short pulses
US6940447B2 (en) Radar device and method for operating a radar device
JPH075252A (en) Time division type FM radar system
US9213095B2 (en) Combined direction finder and radar system, method and computer program product
US3879732A (en) Multi-directional barrage jamming system
US3685050A (en) Single antenna signal retransmission device
WO2019059217A1 (en) Radar device
JP2000065923A (en) Radar apparatus and control method thereof
RU189079U1 (en) MULTI-FUNCTIONAL INTEGRATED SMALL-SIZE TWO-BANDING RADAR SYSTEM FOR AIRCRAFT
JP2022535331A (en) Coherent multistatic radar system especially for use in vehicles
JP2802671B2 (en) Millimeter wave radar transceiver
US4053892A (en) System for enabling coherent signal processing at a remote receiving station
JP3498434B2 (en) Aperture antenna, antenna driving circuit, and radar device
GB1105758A (en) Short-range radar system
JPH09297174A (en) Multi-beam radar device
JP2964947B2 (en) Time-division radar system
JPS60170777A (en) Synthetic aperture radar
JPH07167948A (en) CW radar device
JP2785418B2 (en) Synthetic aperture radar device
JPH06186321A (en) Multi-beam radar device
JPH0142392B2 (en)
JPH05297130A (en) Secondary monitoring radar device
JPH08105955A (en) Radar equipment
JP2906772B2 (en) Rainfall radar device for flying objects