JPH0283423A - Temperature monitor apparatus to be carried on artificial satellite - Google Patents

Temperature monitor apparatus to be carried on artificial satellite

Info

Publication number
JPH0283423A
JPH0283423A JP23707588A JP23707588A JPH0283423A JP H0283423 A JPH0283423 A JP H0283423A JP 23707588 A JP23707588 A JP 23707588A JP 23707588 A JP23707588 A JP 23707588A JP H0283423 A JPH0283423 A JP H0283423A
Authority
JP
Japan
Prior art keywords
temp
telemetry
sensors
matrix
amn
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
JP23707588A
Other languages
Japanese (ja)
Inventor
Ryuji Sasaki
佐々木 隆二
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.)
NEC Corp
Original Assignee
NEC 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 NEC Corp filed Critical NEC Corp
Priority to JP23707588A priority Critical patent/JPH0283423A/en
Publication of JPH0283423A publication Critical patent/JPH0283423A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To obtain a large number of temp. measuring points with limited channel capacity by selecting a temp. sensor to be used in measurement among a plurality of temp. sensors arranged in a matrix state on the basis of a command and connecting the same to a telemetry transmission system through a control unit. CONSTITUTION:(mXn) temp. sensors a11-amn are arranged in a matrix state and transistors b1-bm, C1-Cn are mutually connected so that one of the temp. sensors a11-amn is connected to a telemetry system apparatus (f) when one of the transistors b1-bm and one of the transistors C1-Cn are respectively brought to a continuity state. It is controlled which of the temp. sensors a11-amn is selected for telemetry, by a matrix control apparatus (d) but this selection is changed by the command input (e) from the outside. The matrix of the temp. sensors a11-amn is the sensor group connected to one channel of telemetry channels and, by increasing (m) or (n), many temp. monitors become possible.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は人工衛星搭載用温度モニタ装置に関する。[Detailed description of the invention] [Industrial application field] The present invention relates to a temperature monitoring device mounted on an artificial satellite.

〔従来の技術〕[Conventional technology]

従来、人工衛星搭載用温度モニタ装置は、センサに一定
の電流を流し、その電圧降下を測定しており、サブコミ
ュテーション機能をそなえていても基本的には、ひとつ
のセンサに対してテレメトリ系の1チヤネルが割当てら
れていた。
Conventionally, temperature monitoring devices mounted on artificial satellites pass a constant current through the sensor and measure the voltage drop.Even if they have a subcommutation function, they basically only perform telemetry for one sensor. 1 channel was assigned.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

上述した従来の人工衛星搭載用温度モニタ装置は、テレ
メトリ系のチャネル容量により温度センナの測定点に限
りがあり、人工衛星の大型化に伴い温度モニタのできな
い機器がでてくるため、異常機器の発見や不具合原因の
究明に支障をきたすという欠点がある。
In the conventional satellite temperature monitoring device described above, the number of measurement points of the temperature sensor is limited due to the channel capacity of the telemetry system, and as satellites become larger, some devices become unable to monitor temperature, so it is difficult to detect abnormal devices. This has the disadvantage that it hinders discovery and investigation of the cause of the problem.

本発明の目的は、テレメトリ系の限られたチャ。The object of the present invention is to solve a limited number of telemetry systems.

ネル容量で多数の温度測定点を得ることができる人工衛
星搭載用温度モニタ装置を提供することにある。
An object of the present invention is to provide a temperature monitoring device mounted on an artificial satellite that can obtain a large number of temperature measurement points with a channel capacity.

〔課題を解決する゛ための手段〕[Means for solving problems]

本発明の人工衛星搭載用温度モニタ装置は、マトリック
ス状に配置された複数の温度センサと、これら複数の温
度センサのうち測定しようとする温度センサをコマンド
により選択しテレメトリ送信系に接続する制御装置とを
備えている。
The temperature monitoring device on board an artificial satellite of the present invention includes a plurality of temperature sensors arranged in a matrix, and a control device that selects a temperature sensor to be measured from among the plurality of temperature sensors by a command and connects it to a telemetry transmission system. It is equipped with

〔実施例〕〔Example〕

次に、本発明について図面を参照して説明する。 Next, the present invention will be explained with reference to the drawings.

第1図は本発明の一実施例を示すブロック図である。FIG. 1 is a block diagram showing one embodiment of the present invention.

温度センサall〜a□がマトリックス状にm×n個配
置されており、トランジスタb1〜b、とトランジスタ
01〜C0とのそれぞれひとつが導通状態になると温度
センサall〜a、。のひとつがテレメトリ系装置fに
接続されるように温度センサall〜a□及びトランジ
スタb、〜t) rm + C1〜c0が相互接続され
ている。トランジスタb!〜b、、c1〜C0のオンオ
フはマトリックス制御装置によりコントロールされてい
る。たとえば、トランジスタb1及びclが導通状態の
時は温度センサallにテレメトリ系装置fから一定の
電流がサンプル時に流れ、その電圧降下がテレメトリ系
装置jfのひとつのチャネルに入力され、テレメトリ出
力gとして出力される。マトリックス状の温度センサa
ll〜a、fiのどれをテレメトリすべく選ぶかはマト
リックス制御装置fによりコントロールされるが、これ
は外部からのコマンド人力eにより切替えられるように
なっている。温度センサall〜a□のマトリックスは
テレメトリチャネルの1チヤネルに接続されているセン
サ群であり、テレメトリ系装置fに温度測定用として入
力チャネルがh個割当てられているとしたら、同様のマ
トリックスをh組備えることによりmxn×hの温度モ
ニタが可能であり、hがテレメトリ系装置fのチャネル
数により制限されるとしても、m及びnを大きくとるこ
とにより、多くの温度モニタが可能である。
Temperature sensors all to a□ are arranged in a matrix (m×n), and when each of transistors b1 to b and transistors 01 to C0 becomes conductive, temperature sensors all to a are activated. Temperature sensors all~a□ and transistors b,~t)rm+C1~c0 are interconnected such that one of them is connected to the telemetry system f. Transistor b! The on/off of ~b, , c1~C0 is controlled by a matrix control device. For example, when transistors b1 and cl are conductive, a constant current flows from the telemetry system f to the temperature sensor all during sampling, and the voltage drop is input to one channel of the telemetry system jf and output as the telemetry output g. be done. Matrix temperature sensor a
Which of ll-a and fi is selected for telemetry is controlled by the matrix control device f, which can be switched by an external command e. A matrix of temperature sensors all to a□ is a group of sensors connected to one telemetry channel, and if h input channels are assigned to telemetry system f for temperature measurement, a similar matrix is It is possible to monitor temperatures of mxnxh by providing a set of 2. Even if h is limited by the number of channels of the telemetry system f, by setting m and n large, it is possible to monitor a large number of temperatures.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明は、テレメトリ装置の入力チ
ャネルにコマンドにより切替え可能な温度センサ群のマ
トリックスを接続することにより、限られたテレメトリ
チャネル数で多くの温度測定点を得ることのできる効果
がある。
As explained above, the present invention has the effect of being able to obtain many temperature measurement points with a limited number of telemetry channels by connecting a matrix of temperature sensor groups that can be switched by commands to the input channels of a telemetry device. be.

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

第1図は本発明の一実施例を示すブロック図である。 all〜a0・・・温度センサ、b1〜b、・・・トラ
ンジスタ、C!〜c8・・・トランジスタ、d・・・マ
トリックス制御装置、e・・・コマンド入力、f・・・
テレメトリ系装置、g・・・テレメトリ出力。 町tフ
FIG. 1 is a block diagram showing one embodiment of the present invention. all~a0...Temperature sensor, b1~b,...Transistor, C! ~c8...Transistor, d...Matrix control device, e...Command input, f...
Telemetry system equipment, g...Telemetry output. town tfu

Claims (1)

【特許請求の範囲】[Claims] マトリックス状に配置された複数の温度センサと、これ
ら複数の温度センサのうち測定しようとする温度センサ
をコマンドにより選択しテレメトリ送信系に接続する制
御装置とを備えたことを特徴とする人工衛星搭載用温度
モニタ装置。
An artificial satellite-mounted satellite characterized by comprising a plurality of temperature sensors arranged in a matrix, and a control device that selects a temperature sensor to be measured from among the plurality of temperature sensors by a command and connects it to a telemetry transmission system. temperature monitoring device.
JP23707588A 1988-09-20 1988-09-20 Temperature monitor apparatus to be carried on artificial satellite Pending JPH0283423A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23707588A JPH0283423A (en) 1988-09-20 1988-09-20 Temperature monitor apparatus to be carried on artificial satellite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23707588A JPH0283423A (en) 1988-09-20 1988-09-20 Temperature monitor apparatus to be carried on artificial satellite

Publications (1)

Publication Number Publication Date
JPH0283423A true JPH0283423A (en) 1990-03-23

Family

ID=17010045

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23707588A Pending JPH0283423A (en) 1988-09-20 1988-09-20 Temperature monitor apparatus to be carried on artificial satellite

Country Status (1)

Country Link
JP (1) JPH0283423A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010073396A1 (en) 2008-12-26 2010-07-01 三菱電機株式会社 Operation control device
JP2011095087A (en) * 2009-10-29 2011-05-12 Seiko Epson Corp Temperature sensor and method of detecting temperature
JP2012230039A (en) * 2011-04-27 2012-11-22 Seiko Epson Corp Temperature sensor
JP2012230038A (en) * 2011-04-27 2012-11-22 Seiko Epson Corp Temperature sensor
CN104075822A (en) * 2014-06-12 2014-10-01 上海微小卫星工程中心 Temperature processing device and method in satellite thermal test

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6154412A (en) * 1984-08-24 1986-03-18 Canon Inc Detecting device

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6154412A (en) * 1984-08-24 1986-03-18 Canon Inc Detecting device

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010073396A1 (en) 2008-12-26 2010-07-01 三菱電機株式会社 Operation control device
EP2372329A1 (en) * 2008-12-26 2011-10-05 Mitsubishi Electric Corporation Operation control device
EP2372329A4 (en) * 2008-12-26 2013-03-20 Mitsubishi Electric Corp Operation control device
US8589021B2 (en) 2008-12-26 2013-11-19 Mitsubishi Electric Corporation Operation control device
JP2011095087A (en) * 2009-10-29 2011-05-12 Seiko Epson Corp Temperature sensor and method of detecting temperature
JP2012230039A (en) * 2011-04-27 2012-11-22 Seiko Epson Corp Temperature sensor
JP2012230038A (en) * 2011-04-27 2012-11-22 Seiko Epson Corp Temperature sensor
CN104075822A (en) * 2014-06-12 2014-10-01 上海微小卫星工程中心 Temperature processing device and method in satellite thermal test

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