JPS5879176A - Data correction system of radar apparatus - Google Patents

Data correction system of radar apparatus

Info

Publication number
JPS5879176A
JPS5879176A JP56177943A JP17794381A JPS5879176A JP S5879176 A JPS5879176 A JP S5879176A JP 56177943 A JP56177943 A JP 56177943A JP 17794381 A JP17794381 A JP 17794381A JP S5879176 A JPS5879176 A JP S5879176A
Authority
JP
Japan
Prior art keywords
radar
artificial
antenna
data
earth
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
JP56177943A
Other languages
Japanese (ja)
Other versions
JPH0227629B2 (en
Inventor
Kenichi Inamiya
健一 稲宮
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 JP56177943A priority Critical patent/JPS5879176A/en
Publication of JPS5879176A publication Critical patent/JPS5879176A/en
Publication of JPH0227629B2 publication Critical patent/JPH0227629B2/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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/40Means for monitoring or calibrating

Landscapes

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

Abstract

PURPOSE:To achieve a correct interpretation of data with an easy comparison of image data with an artificial satellite and a radar by receiving a transmitted wave from the same transmission source and an echo signal from the same zone with the artificial satellite and the radar. CONSTITUTION:As an artificial satellite 1 reaches almost right above an antenna 32 of a ground radar, a radar of the satellite is made to synchronize with the ground radar through an antenna 36 or the like of a tracking radar while a microwave is transmitted to the surface of the earth from an antenna 36 with the directivity matching the azimuth. An echo signal formed in the same zone on the surface of the earth is received with a radar of the satellite 1 while done with the antenna 32. Both image data based on the transmitted wave from the same transmission source and the echo signal from the same zone are compared easily thereby enabling an easy and accurate interpretation of data and a highly accurate correction of data.

Description

【発明の詳細な説明】 この発明は人工衛星に招11祝烙〕1.たレーダ装置の
11M (Nデータと地球上の源星デ〜りの楔止の方式
VC関す乙ものである。
[Detailed Description of the Invention] This invention is an artificial satellite. This is a VC related to the method of wedging the 11M (N data) of the radar equipment and the source star data on the earth.

(i) 人T1有星に搭載これたレーダ装置の典d1す的な例と
]〜てマイクロ波散乱61ケ用いて以下の説明を行なう
。マイクロ波L)父乱訂は屯球表面から散乱したマイク
ロ波全受信1.、−tli2球表面の状態全装σ(りし
ようとする。その蜆側原鉗!を簡「1シに図全+i1い
て1以丁に説明する。第11ン1はへT衛星の移動に1
弔うドツプラ′力里の影響全説明するための図で凌7る
。Ig1Mオイ’111i↑人I[9#J]i、 t2
11d’ t 時曲陵に移動した人工繭星の位j1倉、
 +ニー11は人工衛星の移動Wl”、 l’jl、(
4)’人工弁1h4の1鍔度、 i!51はt時11]
前の面丁点とt lL、1曲佼の人工4IFT星ケ結ふ
距離。
(i) The following explanation will be given using a typical example of a radar device installed on the human T1 planet and microwave scattering. Microwave L) My father's interpretation is the complete reception of microwaves scattered from the surface of the turret.1. , -tli2 The state of the surface of the sphere is to be completely σ(. 1
A diagram to explain all the effects of the mourning Dotsupura'Rikiri is shown below. Ig1Moi'111i↑人I[9#J]i, t2
11d't Artificial cocoon star position j1kura moved to Qureum,
+ Knee 11 is the movement of the satellite Wl'', l'jl, (
4) 'Artificial valve 1h4 1st degree, i! 51 is 11 at time t]
The distance between the previous Mencho point and tlL, the artificial 4IFT star connection of 1 curve.

(61は地表向て゛ある。いま人工:i# !f3.の
対地速度全Vとし1時+i4+ t (’、; IC(
2+のr:r ttTに人工+#i和が+Yy 仙する
とその様ツリ1距離tll&:j’ v t Tありゴ
た人工衛星の商j耕(4)全りと表すと、1也表向(6
1のある点から十秒綬の人工酌屓まT゛の距離(51は
(61 is facing the ground surface. Now, the ground speed of artificial: i # ! f3. is all V and 1 o'clock + i4 + t (', ; IC (
2+ r:r ttT has artificial +#i sum +Yy, and when it is 1 distance tll &:j' v t T, the quotient of the artificial satellite is (4) If expressed as all, 1ya obverse (6
The distance from a certain point in 1 to the artificial distance of 10 seconds is T゛ (51 is.

V鮎”1−(Vロ  1゛ある。V sweetfish"1-(Vro  1゛There is.

これを・BfIN1微分すると V2t/仝9を掛る。When this is differentiated by ・BfIN1, it is multiplied by V2t/仝9.

」茄の時:tJl倣分とドツプラ霊位が比例するので。” At the time of eggplant: tJl imitation and Dotsupura spiritual position are proportional.

(2) この式は1呵星ヴ)(曾1gが移11山すると、ドノフ
′うの周波数も’1%なること全ボしている。第2図V
」人工衛星山?真上から兄lこ図て人二に盾Ji!(,
1+ IrL進行方向(81に移動する。人工AtfJ
lj を月の、1rヨ行力向(81(1M角な方向朋に
はドツプラ〃ノ求はシ首生しない。
(2) This equation shows that when 1g moves to 11 points, the frequency of Donov's also becomes 1%. Figure 2 V
” Satellite mountain? My brother is standing directly above me and I am shielding him! (,
1+ IrL traveling direction (move to 81. Artificial AtfJ
If lj is the moon's 1r yaw force direction (81 (1M square direction), no Dotsupra request will occur.

一般にマイクロ波散乱^:は方向(1111に角度成分
全持つ方向(91に対してパルス状の重力を送信し。
In general, microwave scattering ^: transmits a pulse-like gravitational force to a direction (91) that has all angular components in the direction (1111).

」粗球表面で散乱した’;6 ’IA力シケ出び人1箱
++tr ilr tt+で受信する装置である。方間
(1)1のみVC’llf、鼓を送(gする方法は送信
アンテナの111向性全1・IIJI+することにより
実現できる。送信θ■1人Ci4’r 11. t I
 lの面下点から方向+91 Kある距V]11の軸回
1゛曲球に面ケ照躬する。第3図にマイク1]θす1j
ダ乱計が1114人面を観で1すする原子を示す。送1
..波0,1はF点的・甲(、i 1 。
``Scattered on the surface of a rough sphere''; 6 ``This is a device that receives 1 box of IA power output + + trilr tt+. Direction (1) 1 only VC'llf, the method of sending (g) can be realized by transmitting antenna's 111 directivity all 1 IIJI +. Transmission θ ■ 1 person Ci4'r 11. t I
The surface is compared to a curved sphere with an axis rotation of 1° at a distance V]11 in the direction +91 K from the point below the surface of l. In Figure 3, microphone 1] θs 1j
The da random meter shows 1114 human faces and 1 sip of atoms. Send 1
.. .. Waves 0 and 1 are at point F (, i 1 ).

アンテナ半値り届を示す線(111とlI21によって
曲まね。
The line indicating the antenna half price (curved by 111 and lI21).

た立体三角形の〕底辺である地〕ボ人面十?l1((躬
する。これは肋球表面十では力量(9)の両1則に引か
れた(IIど(14)の地域である。12′、悄彼に1
この地1成分同一のパルス波でl(i躬するが、方向l
1l−C示されたΔ原子の谷7.′i+、(’)jlえ
VJ’、’ lI51 、 (I[ilなとか1−11
府)+Elへの(3) 直距離は異なるため、各点から受信される敗乱疲は異な
ったドツプラ変移全党けるので、散古りしたn屑に応し
て受信周波数がj4なってぐる。
The ground which is the base of the three-dimensional triangle is Bojinmen ten? l1 ((True. This is the region of (II) (14) drawn by both the first law of power (9) on the surface of the costal sphere. 12', 1 to him
At this point, one component of the same pulse wave
1l-C Valley of Δ atoms shown 7. 'i+, (')jl え VJ', ' lI51 , (I [il nataka 1-11
(3) Since the direct distances to +El are different, the defeat fatigue received from each point has a different Dotsupura transition, so the reception frequency changes according to the scattered n scraps. .

受信周波数Vi直丁点(71から方向(9)でボ烙tシ
る線の延長士の谷点に応じて連続で変化するが9通常の
マイクロ波散乱哨では方向(91の線上の位1症K 応
U チ一定圧Kf 15 VCm域の区分1f151.
 tliil、 f1’/I。
The reception frequency Vi changes continuously according to the valley point of the extension line of the line that radiates in the direction (9) from the direct point (71). K response constant pressure Kf 15 VCm area division 1f151.
tliil, f1'/I.

+181.1i9i、 12LIl、 (,711,7
21のり+−+ < ?’Tない、受信[双で周波数升
別を行なう。第4図にマイクロ波h 乱n t’の受信
部を示す。第4図においてアンテナ12J1は送信およ
び受信に使用ネれる。このアンテナC3)で受信された
人力はサーギ、レータ(あるいdダイプレクサ例で送受
波が分配をれ、受信部ゐ)で周波数がローカル周波数に
変侠プれて1分配回路(イ)1で分割が行なわれるその
或フィルタU?+ 。
+181.1i9i, 12LIl, (,711,7
21 glue +-+ <? 'T not, receive [frequency separation is performed on both sides. FIG. 4 shows a receiving section for the microwave h disturbance n t'. In FIG. 4, antenna 12J1 is used for transmission and reception. The human power received by this antenna C3) is divided into transmitting and receiving waves using a sergi or a diplexer (for example, a D diplexer), and the frequency is changed to a local frequency in the receiving section (2). That certain filter U on which the division is performed? +.

121i1から(2))を通、遇するが1人力Vは党1
〜時に受Cすているドツプラ変f¥に応じて個有のフィ
ルタを通過する。フィルタを通過しfc他信号企成回路
t:(Oiでチャンネル別[1収出はれ、データ伝送[
す1シ各(31〕?曲して送信回路?経由して1也−し
に送信され(4) る。
121i1 to (2)), but one person V is party 1
The signal passes through a unique filter depending on the Doppler variation f¥ that is being received. Pass through the filter, fc and other signal forming circuits t: (Oi for each channel [1 output, data transmission [
Each signal (31) is transmitted via the transmitting circuit (4).

さて人工酌星山から1兄16111されたデータは信号
処理を行ない画側点の自律デー々を得る。この1而1象
データから観a+++点の状?Mを止しく刊11)(す
る為には、あらかじめ分−〕1いる苅宋・向からの画(
4デ一タ′It手+JiJに多数取1i) 1.、て」
・・き1画像データの解釈?容易にしておく必要がある
。使って地上のある特定地賊全人工+Lli星(11で
、t3?、測すると同時に、その池域ケ同−11.’l
刻にレータ−、1lli口!11′1゜航望1傭、観測
気tボ會使月11〜だ蜆側全行なってデータ全俄侍する
。この両方からly r<j したデータケ比眩し1画
1象テータの解釈が容易にできるよう準備全行なってお
く。しかる波9人工1竹星から+a 1+された朋11
象データの、7Hから止1−く1也球上の状態4111
0丁rきるようになる。
Now, the data received from the artificial Mt. 16111 is subjected to signal processing to obtain autonomous data of the image side points. What is the state of a+++ point based on this 1/1 elephant data? 11) (To do so, please take a few minutes in advance.
4 data 'It hand + JiJ take many 1i) 1. ,hand"
...Ki1 Interpretation of image data? It needs to be made easy. Use a certain bandit on the ground to measure all the artificial + Lli stars (at 11, t3?, and at the same time measure the pond area - 11.'l)
A minute later, 1lli mouth! 11'1° Navigation 1st, observation meeting from 11th month, I went all the way to the Sage side and attended all the data. All preparations have been made so that the data obtained from both of these data can be easily interpreted. Shikuru Wave 9 Artificial 1 Tomo 11 +a 1+ from Takesei
State 4111 of the image data on the 1-1 ball from 7H
You will be able to cut 0 cinch.

しかしながら従来の人工傳Jiとto)上で覚11Mさ
れたデータの比′眩では9両方[Ii、lいられている
1m fil1手段が異なるので、同−池喰に対する1
1況61リデータへの表れ方が>(なり比戴が容易T゛
ない。
However, in the comparison of the data calculated on the conventional artificial image Ji and to), the 1 m fil1 means used for both [Ii, l and 1 m fil1 are different;
The way it appears in the 1st situation 61 redata is not easy to compare.

この発明では観測しようとするI11! 、を或を人工
1竹(5) 星と地上装置とで同一の信寸諒を用いて疲側し。
This invention attempts to observe I11! , or an artificial one (5) The star and the ground equipment use the same reliability.

人工1考星で1替られたデータの解釈が容易にできるよ
うにしたレーダ装置のデータ校正方式を提供するもので
ある。
The present invention provides a data calibration method for a radar device that allows easy interpretation of data that has been changed by one artificial star.

以下この発明の一実施例を図面により詳述する。An embodiment of the present invention will be described in detail below with reference to the drawings.

第51z1はこの発明の一実施例?示す図で、第5図に
おいて(a2+は人工向星山のelぼ直下点に置かれた
アジマス方向に指向9會持つアンテナ全備えた受信装置
のRF部、(幽は信号処理部、(3ωは受信装置と追跡
管制部ケつlぐデータ回線。
Is No. 51z1 an example of this invention? In Fig. 5, (a2+ is the RF section of the receiving device equipped with an antenna with 9 antennas oriented in the azimuth direction, which is placed directly below the el of the artificial Mt. A data line connecting the receiving device and the tracking control unit.

a5:は追跡・d訓の信号処理部、 1J61FI追〃
)・管制用のアンテナ、 +371は下り回線、 +3
81は上り回線である。
A5: Signal processing section for tracking and d-training, 1J61FI tracking
)・Antenna for control, +371 is downlink, +3
81 is an uplink.

きていま人工隋星山が軌道士全移!、11 Lながら観
測を行なっており9人工衛星(11が受信装置濯(32
)の直上附近を通過するとし、かつこの時地表面方向(
131と(14)にパルス状の送信全行なっているとす
7′L1は、受信装置のRF部(3カのアンテナの指向
を人工衛星111のアンテナの半1直幅を示す地表面方
向(]3)と(141に向けて人エイ考星(11の受信
vk受信する。人工衛星山から送信これ、受イぎ装置(
34に(6) 受信ζtLる伝ばん、評路kj’ 、  +Ifx 1
面の反射地点によって点が尾生ずる。
Now, the artificial Sui Xing Mountain has completely relocated its orbiters! , 11 L, but 9 artificial satellites (11 are equipped with receivers (32
), and at this time the direction of the ground surface is (
131 and (14), 7'L1 is the direction of the RF section (three antennas) of the receiving device in the direction of the ground surface (which indicates half the direct width of the antenna of the artificial satellite 111). ] 3) and (towards 141, receive the reception vk of 11. This is transmitted from the artificial satellite mountain, and the receiving device (
34 (6) Reception ζtL transmission, evaluation route kj', +Ifx 1
A point tail is generated depending on the reflection point on the surface.

弔3図でこの関保を触1明−4−ると、圀えL丁人工1
有星山から送信をれ地点flail−(j反射ジれ受信
装置が置かれている人工fI′#r星の直下点lli点
(′11に11ri<送信波の伝ばん時rfji ld
 、回し大王+:?7星(11かI−1回時[送信智れ
1山、貞凹1で)又別さノじ0才に1ス伯゛彼の伝ばん
時1’+、i1より短い。このようV(つ1  ’、’
W、’、 1.’j装置自゛のl伊那!32+は人工隋
却;11から送イ、1智)tTきたパルス状の送信波が
あたかイ、レーダのエコーイ、:1号のように、広がっ
た”’F 1it1幅の間(/(堂イ、−1づJしる。
When you touch this Sekiho in the funeral scene 3, you will see the artificial 1
Point flail-(j Point directly below the artificial fI'#r star where the reflection deflection receiver is placed lli point ('11 to 11ri<When the transmitted wave propagates rfji ld
, Mawashidaio+:? 7 stars (11 or I-1 times [transmission knowledge 1 mountain, Sadoko 1]) Matabetsu also 0 years old 1 stage count, his transmission time 1'+, shorter than i1. Like this V(tsu1','
W,', 1. 'J device's own lina!' 32+ is an artificial disturbance; sent from 11, 1 wisdom) tT The pulse-shaped transmission wave is hot, radar echo, spread like No. 1"'F 1it1 width (/(do I, -1 zu J sign.

信号処理部j331 VC必安な人工1・4JJ+N1
1の込(1−+タイミングは追llll−宙訓月1アン
テナt:1lil ?i−]由じ1下り1111 、仇
伯号の−141≦VC含ませて、データ回線+3111
 ’(+−曲じてJ受イ;イすることができる。
Signal processing section j331 VC essential artificial 1.4JJ+N1
1 (1-+timing will be added lllll- Soukokugetsu 1 antenna t:1lil ?i-) Yuji 1 downlink 1111, including -141≦VC of Qibo, data line +3111
'(+-You can bend J and A; A.

この込イgタイミングは伝t、1′んll:「1it1
のtlN延を補償する必要のある時v、1タイミンク−
4−L7Lめlこブレトリガにすることが1゛きる。1
−タν14 、jlli 7″11X(、Iiaでは送
イ^タイミングと受1.−j装圃(席)で受11jシた
波形より、レーダ受信波1乏と同一の処即ができる。例
(7) えば人工俯星(11の′アンテナの半値幅+1:(lと
(141の間の地表面から反射された信号よI’) C
RT上にPP1画面を作ることができる。このP [−
’ r画面を写真あるいは信号として保存し、同時に同
じ地点全人工衛星によって疎開したデータケ叔傅し、比
較することができる。
This included timing is t, 1'nll: "1it1
When it is necessary to compensate for the tlN extension of v, 1 timing -
4-L7L can be used as a trigger. 1
- data ν14, jlli 7"11X (, in Iia, from the transmission timing and the waveform received at the receiving field (seat), the same treatment as the radar reception wave 1 deficiency can be obtained. Example ( 7) For example, an artificial star (half width of antenna 11' + 1: (signal reflected from the ground surface between l and (141) I') C
You can create a PP1 screen on RT. This P [-
'r Screens can be saved as photos or signals, and data from all satellites evacuated to the same location can be collected and compared at the same time.

なお、頃上の説明では受イぎh *、 caz+ ta
単に地球上に設置されるとしたが、地プボ上の種々の場
所に+*<ことによって神々のf1点を借る。例えば陸
上の商いところに設置することによって受信装置の4.
Al枝が拡大できる。抗空賊に塔載した場合はかなりの
冒度′ft得るので、より一層の横域の拡大が期待でき
る。また船引号利j旧した場合に、大型の装置の搭載か
りnヒで大をアンテナと低碓音増幅益により受信電力の
増大が期待できる。また同時にa箇Ph丁設宵するごと
によって広範囲にわたるデータ比散ができる。当然のこ
とながら覗測の対象となっている地1威を1例えは削土
であれはめ柿Illブイ等の他の方法で画側したデータ
の利用を行なうことにより’46111テータの(8) 解釈がより正確にできる。
In addition, in the explanation above, ukeigi h *, caz + ta
Although it is assumed that it is simply installed on the earth, the f1 point of the gods is borrowed by +*< in various places on the earth. For example, by installing the receiving device at a commercial location on land, 4.
Al branches can be expanded. If mounted on anti-air pirates, it will gain a considerable amount of attack power, so it can be expected to further expand its territory. In addition, if the ship's power is reduced, it is expected that the received power will be increased by installing a large device and using a large antenna and a low amplification gain. Moreover, by setting up a number of Ph.D. at the same time, data can be distributed over a wide range. Naturally, by using the data obtained by other methods such as excavating the ground, which is the target of observation survey, by using other methods such as buoys, etc. Interpretation can be more accurate.

マイクロ波散乱i1と受(F〆!li<?の(受信波1
t、J’ l」標地帯における散乱方間の5゛4斤−2
た方向から発生したエコー信号である。このため1両片
の比較ケ行なう場合、多少の2丁が冗牛す56.ことが
(・)ると老えられるカニ、目上“X IIII !H
>のイ又j二1白なモナル全1・jj々の覗租[精米よ
り伯−1戊す)1. l;J’ 、  マイクロ波1孜
乱訂と受イぎ装装置の双15の受イ「−彼ケ理論的に、
−11iひ付けることかでes、 −+慎牧1Fカ法の
I*1.itが同上する。
Microwave scattering i1 and receiving (F〆!li<? (received wave 1
5゛4 catty-2 between the scattering directions in the t, J'l'' marking zone
This is an echo signal generated from the opposite direction. For this reason, when comparing one piece, some two pieces are redundant.56. The crab that gets old when things happen (・), the superior “XIII!H
>のImataj21 White Monal All 1・jj's Preview [Haku-1 from Polished Rice] 1. l;J', Microwave 1. Theoretically,
-11i Hitekutoka de es, -+Shinmaki 1F Kaho I*1. It is same as above.

以十のように、この究明(’(’I;1′Lる01!6
川力を去を月1いて、同−池帯全回一送1i′諒の込(
、−f波の反射により発生したエコーh5弓否べ−L 
11I」星(11と受信装置lL+:121によって受
信し、双方より111目家データをtgて9両者r比吹
できるので1人]−1rlII)i!からrl、42 
flll+されたデータの解釈がより+1.11n+ 
vc出」(る利点が・りる。
As in the above, this investigation ('('I;1'Lru01!6
After leaving Kawa Riki once a month, I sent all the episodes in the same month.
, -Echo h5 generated by reflection of f wave -L
11I'' star (11 and receiving device lL+: received by 121, tg the 111th house data from both sides, and can compare 9 both r, so one person] -1rlII) i! from rl, 42
The interpretation of full+ data is +1.11n+
VC output"

【図面の簡単な説明】 第1図は人工術星の4−イ動に伴うドツプラ幼果を説明
するための図、第2図〃、1人王Hi星k pri星(
9) の直上よりみた1ンl、@3図はマイクロ波散乱削プに
地表面を観測する面子を示す図、第4図はマイクロ波散
乱削の受イぎ都ケ示すブロック図、第5図はこの発明に
係る′央弛し1]ケ示す図である。 図中(月は人工両組、l、4+Id人工1.町星の高!
糺(61は地表面、 ono2・はア〕/テナの1÷埴
輻を示す線。 I13・(I4)は他表面力量 1.321は受1呂民
if7のRFバB 、 I531は受1ぎ装置の惰−弓
Iか1既 (34)は戸−夕回線、  r+:は3J3
跡肯訓部の信号処理t□1)、(釧tま」μ跡官制部の
アンテナ、 !3’/lは下り回線、 !3ijl 6
11−り回線である。 なお、1ヌ1中の一部分あるいに1目当部分には同一の
符号が付しである。 代理人 島 封 伯 − (lO)
[Brief explanation of the drawings] Figure 1 is a diagram to explain the Dotsupura immature resulting from the 4-i movement of the artificial star.
9) Viewed from directly above, Figure 1 is a diagram showing the aspect of observing the ground surface using microwave scattering. Figure 4 is a block diagram showing the main areas for microwave scattering. The figure is a diagram illustrating the 'center relaxation 1' according to the present invention. In the figure (the moon is artificial both groups, l, 4 + Id artificial 1. Town star high!
糺 (61 is the ground surface, ono2・is A) / Tena's 1 ÷ Hanai line. I13・(I4) is the other surface ability 1.321 is the RF bar B of Uke 1 Romin if7, I531 is Uke 1 (34) is a door-to-evening line, r+: is 3J3
Signal processing of the Atoken Training Department t□1), (Kushitma'μ) Antenna of the Ato Government Administration Department, !3'/l is the downlink, !3ijl 6
11-ri line. In addition, the same reference numerals are attached to a part of 1-nu 1 or the 1st target part. Agent Haku Shima - (lO)

Claims (1)

【特許請求の範囲】 人工++47星に塔載烙れ、地球表面にマイクロ波ケ送
信し、かつ地J求表面の11父乱エコーを受信するレー
タ装置と、地球上に設置きれかつ人工呵星のは(・γ商
丁点に置かれたアジマス方向に指向性を持つアンテナを
有する受信装置と全備え。 」二記人f南星が1:記受信装置首のuIJ−附近に桟
1萌したとき、上記受信装置のアンテナを上記11球表
面方向に指間ζせて上i尼池球表面で1枚乱したエコー
ケ上記し−ダ装酋も・よび受信装置で受信することによ
り画像データを得るようになし。 その鏝両首の画1象テータを比較すること全特徴とする
レーク装置のデータ仮止方式。
[Claims] A radar device installed on an artificial ++47 star, transmitting microwaves to the earth's surface, and receiving 11 echoes from the earth's surface, and an artificial star installed on the earth. It is fully equipped with a receiving device that has an antenna with directivity in the azimuth direction placed at the gamma commercial point.'' When the second recorder F Nansei placed a crosspiece near the receiving device's neck, uIJ-1. , the antenna of the receiving device is moved in the direction of the surface of the 11th ball, and one piece of echo is disturbed on the surface of the 11th ball. The data temporary fixing method of the rake device is characterized by comparing the image data of both heads of the iron.
JP56177943A 1981-11-06 1981-11-06 Data correction system of radar apparatus Granted JPS5879176A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP56177943A JPS5879176A (en) 1981-11-06 1981-11-06 Data correction system of radar apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP56177943A JPS5879176A (en) 1981-11-06 1981-11-06 Data correction system of radar apparatus

Publications (2)

Publication Number Publication Date
JPS5879176A true JPS5879176A (en) 1983-05-12
JPH0227629B2 JPH0227629B2 (en) 1990-06-19

Family

ID=16039779

Family Applications (1)

Application Number Title Priority Date Filing Date
JP56177943A Granted JPS5879176A (en) 1981-11-06 1981-11-06 Data correction system of radar apparatus

Country Status (1)

Country Link
JP (1) JPS5879176A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103675775A (en) * 2013-12-12 2014-03-26 北京理工大学 Method for analyzing influences of background ionosphere on GEO SAR imaging

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102335274B1 (en) * 2019-09-22 2021-12-06 (주) 솔리렉스 Wearable musculoskeletal guard
KR102335273B1 (en) * 2019-10-06 2021-12-02 이종성 X-bend type wearable musculoskeletal guard

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103675775A (en) * 2013-12-12 2014-03-26 北京理工大学 Method for analyzing influences of background ionosphere on GEO SAR imaging
CN103675775B (en) * 2013-12-12 2016-01-20 北京理工大学 Background ionosphere is to the analytical approach of GEO SAR Imaging

Also Published As

Publication number Publication date
JPH0227629B2 (en) 1990-06-19

Similar Documents

Publication Publication Date Title
US4214244A (en) Null pattern technique for reduction of an undesirable interfering signal
CN108535744B (en) Intelligent forwarding type navigation deception method and equipment based on aircraft
US3171126A (en) Passive detection and ranging system
JP2016524704A (en) Method for locating a target and multistatic radar system for realizing such a method
Harness et al. A study on SAR noise jamming and false target insertion
Jezek et al. Two-frequency radar experiments for sounding glacier ice and mapping the topography of the glacier bed
JPH0312711B2 (en)
Sherstyukov et al. Collocated ionosonde and dense GPS/GLONASS network measurements of midlatitude MSTIDs
Vierinen et al. Multi-instrument observations of the Pajala fireball: Origin, characteristics, and atmospheric implications
JPS5879176A (en) Data correction system of radar apparatus
JP5171517B2 (en) Image radar device
Berngardt et al. ISTP SB RAS DECAMETER RADARS
Phillips et al. The Apollo 17 lunar sounder
Lind et al. First passive radar observations of auroral E‐region irregularities
FR2819657B1 (en) METHOD AND DEVICE FOR LOCATING A TERRESTRIAL TRANSMITTER FROM A SATELLITE
Galushko et al. Bistatic HF diagnostics of TIDs over the Antarctic Peninsula
Hofstee et al. Ion-acoustic waves and aspect sensitivity in radio aurora
Kolomiyets Uncertainties in MARS meteor Orbit radar data
JPS61193088A (en) Synthetic aperture radar equipment
Munton et al. A midlatitude HF propagation experiment over New Mexico
Mandal et al. IRNSS capabilities: An initial study using IGS receiver
Afraimovich et al. Instantaneous response of the ionosphere to a sudden commencement of the strong magnetic storm of April 6, 2000
Malcolm Electron Echo 6-a Study by Particle Detectors of Electrons Artificially Injected Into the Magnetosphere.
Herman et al. Picosatellite identification and Doppler estimation using passive radar techniques
Hennessy Surveillance of Space with Passive Radar using the Murchison Widefield Array