JPS61209362A - Multichannel microwave radiometer - Google Patents

Multichannel microwave radiometer

Info

Publication number
JPS61209362A
JPS61209362A JP60049933A JP4993385A JPS61209362A JP S61209362 A JPS61209362 A JP S61209362A JP 60049933 A JP60049933 A JP 60049933A JP 4993385 A JP4993385 A JP 4993385A JP S61209362 A JPS61209362 A JP S61209362A
Authority
JP
Japan
Prior art keywords
noise source
channel
temp
switch
receiver
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
JP60049933A
Other languages
Japanese (ja)
Inventor
Kenji Teshigawara
勅使河原 犬二
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 JP60049933A priority Critical patent/JPS61209362A/en
Publication of JPS61209362A publication Critical patent/JPS61209362A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To reduce the outer shape dimension, wt. and power consumption of a radiometer, by using a multichannel comparing noise source in the correction of the high temp. side of a multichannel microwave radiometer and making it possible to use said noise source in common to each channels. CONSTITUTION:When the switch SW8 of a channel chB is connected to a (3)-side, the noise temp. of a multichannel comparing noise source B is guided to a receiver 10 and voltage V0 is generated in the receiver 10. Next, the switch SW8 of the channel chB is changed over from the (3)-side to a (2)-side and, when the switch SW7 of a channel chA is in the (3)-side, correction temp. T1 is guided to the receiver from a dummy load 11 and, when in the (2)-side, the temp. TA of an antenna 1 is guided to the receiver 10 to respectively generate voltages V1, V. Temp. sensors are attached to the noise source 13 and the dummy load 11 to obtain respective input temp. T0 and T1 of the receiver 10. The temp. TA can be calculated from a predetermined formula by using temps. T0, T1 and voltages V0, V1, V. As mentioned above, the noise source 13 is used in a high temp. side correction source to reduce the standard noise source and correction source change-over switch of each channel and, because the noise source 13 is used in common to each channel, one comparing noise can be reduced.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は人工衛星等の飛翔体に搭載してリモートセン
シング(Remote8anaing)を行なう多チャ
ンネルマイクロ波放射計の改良に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to an improvement of a multi-channel microwave radiometer that is mounted on a flying object such as an artificial satellite and performs remote sensing.

〔従来の技術〕[Conventional technology]

まず、従来のこの種の多チャンネルマイクロ波放射計の
うち2チャンネルマイクロ波放射計について説明する。
First, a two-channel microwave radiometer among conventional multi-channel microwave radiometers of this type will be described.

第2図は従来の2チャンネルマイクロ波放射計を示すブ
ロック図であシ、第2図において、(1)は受信アンテ
ナ、(2)は低温側雑音源であるスカイホーン、 13
1 、141はそれぞれ分波器A。
Figure 2 is a block diagram showing a conventional two-channel microwave radiometer. In Figure 2, (1) is a receiving antenna, (2) is a skyhorn which is a low temperature side noise source, and 13.
1 and 141 are branching filters A, respectively.

B 、 15+は高温側雑音源である標準雑音源、(6
1は比較雑音源、 +71 、 (8) 、 +91 
tiそれぞれスイッチA、B。
B, 15+ is a standard noise source which is a high temperature side noise source, (6
1 is the comparison noise source, +71, (8), +91
ti switches A and B, respectively.

CおよびαQは受信機である。なお131 、141の
分波器A、B以降α・の受信機まではそれぞれのチャン
ネルが同一の構成となっておシ、これをチャンネル人、
チャンネルBとする。
C and αQ are receivers. Note that each channel from the branching filters A and B of 131 and 141 to the receiver of α has the same configuration.
Let's call it channel B.

次に動作原理について、説明の便宜上チャンネルAのみ
について述べる。
Next, regarding the operating principle, only channel A will be described for convenience of explanation.

一般に自然界の物体からは電磁波が放射されておシ、放
射の強度はその物体の輝度温度と密接な関係がある。第
2図の受信アンテナ(11で受信されるアンテナ温度T
Aは、受信アンテナ(ll’i取カまく物体の輝度温度
の分布TB (Ω)と受信アンテナ(11の利得関数G
(Ω)とを用いて。
Generally, objects in the natural world emit electromagnetic waves, and the intensity of the radiation is closely related to the brightness temperature of the object. The antenna temperature T received by the receiving antenna in Fig. 2 (11)
A is the distribution of brightness temperature TB (Ω) of the object surrounding the receiving antenna (ll'i) and the gain function G of the receiving antenna (11).
(Ω) using.

で表わされる。ここでΩは立体角である。It is expressed as Here Ω is the solid angle.

スイッチA(7)が■側に接続されている場合、受信さ
れたアンテナ温度TAは、スイッチ(8)に向かう。ス
イッチB(8)はある瞬間には■側に接続され。
When the switch A (7) is connected to the ■ side, the received antenna temperature TA goes to the switch (8). Switch B (8) is connected to the ■ side at a certain moment.

次の瞬間には、■側に接続される操作全数百Hzで繰シ
返す。またスイッチB(8)の■側には比較的高温で一
定温度Toの雑音を発生する比較雑音源(6)が接続さ
れており、このスイッチ切換操作に同期する受信機αQ
内の同期検波器を通して、比較雑音源(6)の温度To
とアンテナ温度TAO値を知ることが必要条件であり、
この値は受信機+1(1円で発生する出力電圧v’6用
いて次の手順を経ることによって求めることができる。
In the next moment, the operation connected to the ■ side is repeated at several hundred Hz. In addition, a comparison noise source (6) that generates noise at a relatively high temperature and a constant temperature To is connected to the ■ side of the switch B (8), and a receiver αQ that is synchronized with this switch switching operation is connected.
The temperature To of the comparison noise source (6) is measured through the synchronous detector in
It is a necessary condition to know the antenna temperature TAO value.
This value can be found by using the output voltage v'6 generated by the receiver +1 (1 yen) and going through the following procedure.

まずスイッチA(7)の接続を■側から■側に切り換え
る。スイッチC(9)が■側の時にスカイホーン(2)
からのアンテナ温度T1が、セして■側の時に標準雑音
源(5)の雑音温度T2が受信機a1に導かれ。
First, switch the connection of switch A (7) from the ■ side to the ■ side. Sky horn (2) when switch C (9) is on side
When the antenna temperature T1 from the center is on the side (■), the noise temperature T2 of the standard noise source (5) is guided to the receiver a1.

それぞれ比較雑音源(61との温度差に比例した電圧v
1およびv2が受信機ao内で発生する。ここでスカイ
ホーン(2)は常に宇宙冷却空間に向けられているとす
れば、その輝度温度は周波数の関数として既知の量であ
シ、同時にスカイホーン(2)自身の利得関数も既知で
あるため、これら七本とに受信機αGの入力温度T+ 
t”知ることができる。一方標準雑音源]5)の雑音温
度も標準雑音源(5)に温度センサを取シ付け、それを
モニタすることによって受信機aI内の入力温度T2 
t−知ることができる。なおTI <T2<To a 
Vt>V>Vzの関係があ’) a Tl e T2 
sv+ * ”2 およびVがわかるとアンテナ温度T
Aは次式から求まる。
A voltage v proportional to the temperature difference with the comparative noise source (61)
1 and v2 occur within the receiver ao. If the skyhorn (2) is always directed toward the cooling space of space, its brightness temperature is a known quantity as a function of frequency, and at the same time, the gain function of the skyhorn (2) itself is also known. Therefore, the input temperature T+ of the receiver αG for these seven wires is
On the other hand, the noise temperature of the standard noise source (5) can also be determined by attaching a temperature sensor to the standard noise source (5) and monitoring it to determine the input temperature T2 in the receiver aI.
t-can be known. Note that TI < T2 < To a
There is a relationship of Vt>V>Vz) a Tl e T2
If sv+ * ”2 and V are known, the antenna temperature T
A can be found from the following equation.

以上では、説明の便宜上スイッチ等のRF回路の損失は
無いものと仮定している。
In the above description, for convenience of explanation, it is assumed that there is no loss in the RF circuit such as a switch.

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

以上の説明からも明らかなようにスカイホーン(2)と
標準雑音源(31はアンテナ温度TAヲ求めるために用
いられる校正用雑音源であ)、この2つの校正用雑音源
を用いてマイクロ波放射計の校正を行なっている。
As is clear from the above explanation, the skyhorn (2) and the standard noise source (31 is a calibration noise source used to determine the antenna temperature TA) are used to generate microwaves using these two calibration noise sources. The radiometer is being calibrated.

しかしながら、従来のこの多チャンネルマイクロ波放射
計の場合、各チャンネルごとに標準雑音源(5)および
比較雑音源(6)ヲ使用しておシ、また。
However, in this conventional multi-channel microwave radiometer, a standard noise source (5) and a comparative noise source (6) are used for each channel.

スカイホーン(2)と標準雑音源(5)ヲ切り換えるス
イッチ日(8)が必要となるため重量および外形寸法が
大きくなるとともに消費電力が増大し、かつスカイホー
ンは月、太陽および地球の影響を受けない宇宙冷却空間
に向けて配置する必要があるため衛星上での取シ付は位
置が非常に限定されるといった問題点があった。
A switch (8) is required to switch between the skyhorn (2) and the standard noise source (5), which increases weight and external dimensions and increases power consumption. There was a problem in that the mounting position on the satellite was very limited because it had to be placed facing the space cooling space where it would not be exposed to heat.

この発明は、かかる問題点を解決するためになされたも
のであシ多チャンネルマイクロ波放射計の校正源を改良
することによフ外形寸法1重量。
The present invention has been made to solve these problems by improving the calibration source of a multi-channel microwave radiometer.

消費電力を小さクシ、かつ、低温側校正源を衛星上の任
意の場所に取り付けられる多チャンネルマイクロ波放射
計を得ることを目的とする。
The purpose of this project is to obtain a multichannel microwave radiometer with low power consumption and a low-temperature calibration source that can be installed anywhere on the satellite.

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

この発明に係る多チャンネルマイクロ波放射計は標準雑
音源を除去し高温側の校正に多チャンネル比較雑音源を
使用し、かつこの多チャンネル比較雑音源を各チャンネ
ルに共通に使用できる構成とし友ものであシ、さらに、
低温側校正源にサーマルインシュレータに覆われた放射
冷却ダミーロードを使用したものである。
The multi-channel microwave radiometer according to the present invention eliminates the standard noise source, uses a multi-channel comparison noise source for high-temperature side calibration, and has a configuration in which this multi-channel comparison noise source can be used commonly for each channel. Adashi, furthermore,
A radiation-cooled dummy load covered with a thermal insulator is used as the low-temperature side calibration source.

〔作用〕 この発明においては高温側校正源に多チャンネル比較雑
音源信号を使用することによシ各チャンネルの標準雑音
源および校正源を切り換えるスイッチを1つ削減するこ
とができる。
[Operation] In the present invention, by using a multi-channel comparison noise source signal as the high temperature side calibration source, it is possible to reduce the number of switches for switching between the standard noise source and the calibration source for each channel by one.

また、多チャンネル比較雑音源を各チャンネルに共通に
使用しているため比較雑音が1つ削減できる。
Furthermore, since the multi-channel comparison noise source is commonly used for each channel, the number of comparison noises can be reduced by one.

さらに、放射冷却を行なうダミーロードを使用すること
によシ宇宙冷却空間に相当する低温側校正信号を発生さ
せることができる。
Furthermore, by using a dummy load that performs radiation cooling, it is possible to generate a low-temperature side calibration signal that corresponds to the space cooling space.

〔実施例〕〔Example〕

第1図はこの発明の一実施例を示す2チャンネルマイク
ロ波放射計のブロック図であ#)fil〜σOは上記従
来装置と全く同一のものである。αυは放射冷却ダミー
ロード、α3は放射冷却ダミーロード全種い太陽5月、
地球からの熱を防ぐサーマルインシュレータ、(T3は
多チャンネル比較m音源、 (14)u分波器Cである
FIG. 1 is a block diagram of a two-channel microwave radiometer showing an embodiment of the present invention. fil to σO are exactly the same as the conventional device described above. αυ is a radiation cooling dummy load, α3 is a radiation cooling dummy load,
A thermal insulator that prevents heat from the earth, (T3 is a multi-channel comparison m sound source, (14) u duplexer C.

次に動作原理について、説明の便宜上チャンネル人のみ
について述べる。
Next, regarding the operating principle, only the channel person will be described for convenience of explanation.

まず、スイッチB(8)を■側に接続すると、このとき
多チャンネル比較雑音源αυの雑音温度Toが受信機+
l[lに導かれ、受信機(lcI内で電圧VQが発生す
る。
First, when switch B (8) is connected to the ■ side, the noise temperature To of the multi-channel comparison noise source αυ becomes +
A voltage VQ is generated in the receiver (lcI).

次にスイッチB(8)の接続全■側から■側に切り換え
る。スイッチ人(7)が■側のときにダミーロードαυ
からの校正温度T1が、セして■側のときにアンテナ温
度−が受信機に導かれ、それぞれ電圧v1およびVが発
生する。
Next, switch all connections of switch B (8) from the ■ side to the ■ side. Dummy load αυ when switch person (7) is on ■ side
When the calibration temperature T1 from 1 is on the side (2), the antenna temperature - is introduced to the receiver, and voltages v1 and V are generated, respectively.

ここで多チャンネル比較雑音源α3およびダミーロード
αυに温度センサを取り付けることによってそれぞれの
受信機αυの入力温度’r(1および’r+Th知るこ
とができる。なお、 TI < TA < To −V
t > V > T。
Here, by attaching temperature sensors to the multi-channel comparison noise source α3 and the dummy load αυ, the input temperature 'r(1 and 'r+Th) of each receiver αυ can be known.In addition, TI < TA < To −V
t>V>T.

の関係かあ’) e TO* T1 * vos Vl
およびVがわかるとアンテナ温度TAは次式から求まる
relationship?) e TO* T1 * vos Vl
and V, the antenna temperature TA can be found from the following equation.

このように、この考案の多チャンネルマイクロ波放射計
は従来の2つの校正用雑音源音用いた多チャンネルマイ
クロ波放射計と同じ性能を有していることは明らかであ
る。
Thus, it is clear that the multi-channel microwave radiometer of this invention has the same performance as the conventional multi-channel microwave radiometer using two calibration noise sources.

〔発明の効果〕〔Effect of the invention〕

この発明の多チャンネルマイクロ波放射計は以上説明し
たとおシ従来の多チャンネルマイクロ波放射計に比べて
各チャンネルの標準雑音源が不要であ夛、各チャンネル
ごとに切換えスイッチがtつ少ない構成となっている。
As explained above, the multi-channel microwave radiometer of the present invention does not require a standard noise source for each channel compared to conventional multi-channel microwave radiometers, and has a configuration with t fewer switches for each channel. It has become.

また、1つの多チャンネル比較雑音源を各チャンネルに
共通に使用しているため重量、外形寸法および消費電力
が小さいという効果がある。
Furthermore, since one multi-channel comparison noise source is commonly used for each channel, weight, external dimensions, and power consumption are reduced.

さらに放射冷却ダミーロードおよびサーマルインシュレ
ータを使用しているため低温側校正源を衛星上の任意の
場所に取シ付けることができるという効果を有している
Furthermore, since a radiation-cooled dummy load and a thermal insulator are used, the low-temperature side calibration source can be mounted anywhere on the satellite.

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

第1図はこの発明の一実施例を示すブロック図。 第2図は従来の多チャンネルマイクロ波放射計のブロッ
ク図である。 図中、(1)はアンテナ、T2)はスカイホーン、13
1Fi分波器A 、 +41は分波器B 、 +51は
標準雑音源、(6)は比較雑音源、 +71 、 +8
1 、 (91はそれぞれスイッチA。 B、C,(IIH受信機、 (111iタミーCI −
)’ 、 (13ut−マルインシュレータ、αjは多
チャンネル比較雑音源、 +141は分波器Cである。
FIG. 1 is a block diagram showing one embodiment of the present invention. FIG. 2 is a block diagram of a conventional multi-channel microwave radiometer. In the figure, (1) is the antenna, T2) is the skyhorn, and 13
1Fi duplexer A, +41 is duplexer B, +51 is standard noise source, (6) is comparison noise source, +71, +8
1, (91 is switch A, respectively. B, C, (IIH receiver, (111i Tammy CI -
)', (13ut-multi insulator, αj is a multi-channel comparison noise source, +141 is a duplexer C.

Claims (1)

【特許請求の範囲】[Claims] 人工衛星等の飛翔体に搭載され、観測信号を受信するア
ンテナと、上記アンテナからの観測信号を複数のチャン
ネルに分配する分波器と、低温側校正源に使用する放射
冷却ダミロードと、上記ダミロードを覆うサーマルイン
シュレータと、上記ダミーロードからの低温校正信号を
複数のチャンネルに分配する分波器と、上記アンテナと
上記ダミーロードを切り換えるスイッチと、高温側校正
源に使用する多チャンネル比較雑音源と、上記多チャン
ネル比較雑音源からの高温校正信号を複数のチャンネル
に分配する分波器と、アンテナまたはダミーロードと比
較雑音源を切り換えるスイッチと、観測信号を増幅およ
び検波する受信機とを備えたことを特徴とする多チャン
ネルマイクロ波放射計。
An antenna mounted on a flying object such as an artificial satellite to receive an observation signal, a duplexer that distributes the observation signal from the antenna to multiple channels, a radiation-cooled dummy load used as a low-temperature side calibration source, and the dummy load mentioned above. a thermal insulator that covers the dummy load, a duplexer that distributes the low-temperature calibration signal from the dummy load to multiple channels, a switch that switches between the antenna and the dummy load, and a multi-channel comparison noise source that is used as the high-temperature side calibration source. , a duplexer that distributes the high temperature calibration signal from the multi-channel comparison noise source to a plurality of channels, a switch that switches between the antenna or dummy load and the comparison noise source, and a receiver that amplifies and detects the observation signal. A multi-channel microwave radiometer characterized by:
JP60049933A 1985-03-13 1985-03-13 Multichannel microwave radiometer Pending JPS61209362A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60049933A JPS61209362A (en) 1985-03-13 1985-03-13 Multichannel microwave radiometer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60049933A JPS61209362A (en) 1985-03-13 1985-03-13 Multichannel microwave radiometer

Publications (1)

Publication Number Publication Date
JPS61209362A true JPS61209362A (en) 1986-09-17

Family

ID=12844816

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60049933A Pending JPS61209362A (en) 1985-03-13 1985-03-13 Multichannel microwave radiometer

Country Status (1)

Country Link
JP (1) JPS61209362A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20180134458A (en) * 2017-06-08 2018-12-19 국방과학연구소 Apparatus for sensitivity improvement of radiometers by using image frequency bands
CN111273276A (en) * 2018-12-05 2020-06-12 核工业西南物理研究院 Multichannel microwave Doppler reflectometer based on self-excited oscillation microwave source

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20180134458A (en) * 2017-06-08 2018-12-19 국방과학연구소 Apparatus for sensitivity improvement of radiometers by using image frequency bands
CN111273276A (en) * 2018-12-05 2020-06-12 核工业西南物理研究院 Multichannel microwave Doppler reflectometer based on self-excited oscillation microwave source

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