JPS5932600A - Horizon detector - Google Patents

Horizon detector

Info

Publication number
JPS5932600A
JPS5932600A JP57143913A JP14391382A JPS5932600A JP S5932600 A JPS5932600 A JP S5932600A JP 57143913 A JP57143913 A JP 57143913A JP 14391382 A JP14391382 A JP 14391382A JP S5932600 A JPS5932600 A JP S5932600A
Authority
JP
Japan
Prior art keywords
detector
sensor
horizon
earth
analog
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
JP57143913A
Other languages
Japanese (ja)
Inventor
寺西 昭男
松本 幹男
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial Co Ltd
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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP57143913A priority Critical patent/JPS5932600A/en
Publication of JPS5932600A publication Critical patent/JPS5932600A/en
Pending legal-status Critical Current

Links

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、三軸安定化衛星の姿勢を検出する地平線検出
装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a horizon detection device for detecting the attitude of a three-axis stabilized satellite.

従来例の構成とその問題点 従来、三軸安定化衛星に使用される地平線検出装置の赤
外線検出器は、第1図に示すようなアナログ検出器であ
った。すなわち衛星より光学系(図示せず)で地球の像
11を結ばせ、その地平線10が、例えば東西南北に設
置されたサーミスタ、サーモバイル等のアナログ赤外線
検出器(13E、13W、133.13N)にかかるよ
うにする。この時、1つの検出器(例えば13S)に注
目すると、地球11を見ている斜線部分Xと、宇宙12
を見ている部分(1−X)に分かれる。
Conventional Structure and Problems Conventionally, the infrared detector of a horizon detection device used in a three-axis stabilized satellite has been an analog detector as shown in FIG. That is, an image 11 of the earth is formed from a satellite using an optical system (not shown), and the horizon 10 is detected by analog infrared detectors (13E, 13W, 133.13N) such as thermistors and thermomobiles installed in the north, south, east, west, and the like. so that it takes At this time, if you pay attention to one detector (for example, 13S), you can see the shaded area X that is looking at the earth 11, and the space 12
It is divided into the part (1-X) where you are looking at.

今、検出器がすべて地球゛を見た場合(x−1に相当す
る場合)の検出器出力をvE、検出器がすべて宇宙を見
だ場合(x−0に相当する場合)の検出器出力をv6と
すると、検出器13S−7JX第1図に示す位置にある
場合の出力vxは、Vよ−■E−x+ V8(1−x 
)となる。
Now, the detector output when all the detectors see the earth (corresponds to x-1) is vE, and the detector output when all the detectors see the universe (corresponds to x-0) Let v6 be the output vx when the detector 13S-7JX is in the position shown in Fig.
).

定して、地平線位置Xを知ることができる。同様に、検
出器13E、13W、13Nについて求め、検出器13
Eと検出器13Wの出力の差を演算すると、東西方向(
例えばロール軸方向)の傾きを計算できる。同様に検出
器13Sと13Nで南北方向(例えばピッチ軸方向)の
傾きが求まる。
The horizon position X can be determined by Similarly, the detectors 13E, 13W, and 13N are obtained, and the detector 13
When calculating the difference between the output of E and the output of the detector 13W, the east-west direction (
For example, the inclination in the roll axis direction can be calculated. Similarly, the inclination in the north-south direction (for example, pitch axis direction) is determined by the detectors 13S and 13N.

しかし、このアナログ型検出器を用いる方法は、地球の
季節、緯度による赤外線輻射強度の変化および検出器自
体の温度によシ、誤差を生じ、精度よく地平線位置を検
出することが困難であった。
However, this method using an analog detector caused errors due to changes in infrared radiation intensity depending on the earth's seasons and latitude, and the temperature of the detector itself, making it difficult to accurately detect the horizon position. .

発明の目的 本発明は赤外線輻射強度の変化や検出器自体の温度変化
による誤差のない高精度でかつ比較的構成の簡単な地平
線検出装置を得ることを目的としたものである。
OBJECTS OF THE INVENTION The object of the present invention is to provide a highly accurate horizon detection device that is free from errors due to changes in infrared radiation intensity or changes in the temperature of the detector itself and has a relatively simple configuration.

発明の構成 本発明は、精度の必要な線型領域センサとして複数個の
赤外線検出要素よりなるリニアアレイセンサを、捕捉領
域センサとしてアナログセンサを用いるようにしたもの
である。
Structure of the Invention The present invention uses a linear array sensor comprising a plurality of infrared detection elements as a linear area sensor that requires accuracy, and uses an analog sensor as a capture area sensor.

実施例の説明 以下実施例について図面を参照しながb詳細に説明する
。第2図に本発明による地平線検出装置の一実施例を示
す。
DESCRIPTION OF EMBODIMENTS Hereinafter, embodiments will be described in detail with reference to the drawings. FIG. 2 shows an embodiment of the horizon detection device according to the present invention.

第2図において、地球11と宇宙12の境界すなわち地
平線10の像を検出器20に結ばせる。
In FIG. 2, a detector 20 forms an image of the boundary between the earth 11 and the universe 12, that is, the horizon 10.

検出器20は、複数個の赤外線検出要素211で形成さ
れるリニヤアレイセンサ21と、この要素211の出力
を導電体212で取出し、これを読み出すための例えば
シフトレジスタなどの走査機能素子24、宇宙側の捕捉
領域アナログセンサ22、および地球側の捕捉領域アナ
ログセンツー23より構成され1いる。
The detector 20 includes a linear array sensor 21 formed of a plurality of infrared detection elements 211, a scanning function element 24 such as a shift register for extracting the output of the element 211 with a conductor 212, and a space sensor 24 for reading out the output of the element 211. It consists of a capture area analog sensor 22 on the side and a capture area analog sensor 23 on the earth side.

アナログセンサは、前述したごとく検出器自体の温度に
よって出力の絶対値が変化する。しかし、センサ自身を
第3図イに示すように多数の検出器要素211で構成し
た場合、地球の像11を結んでいる検出器要素の出力は
、同図口のdに示すように、宇宙12に相当する同図口
のbに示すものより入射赤外線のエネルギ量に相当する
分(第3図C)だけ大きくなる。各要素の出力aおよび
bは、検出器自体の温度によって変化するが、その差の
信号Cは、地坪゛と宇宙の入射エネルギの差によって決
まるものであるから一定であり同図イに示す地平線10
の像が、このリニアアレイセンサ要素211内のどれか
にある場合は、かならずその境界がどの要素211にあ
るかを決定できる。
As mentioned above, the absolute value of the output of an analog sensor changes depending on the temperature of the detector itself. However, if the sensor itself is composed of a large number of detector elements 211 as shown in Figure 3A, the output of the detector elements forming the image 11 of the Earth will be It is larger than that shown at b in the figure, which corresponds to 12, by an amount corresponding to the energy amount of the incident infrared rays (FIG. 3C). The outputs a and b of each element change depending on the temperature of the detector itself, but the difference signal C is determined by the difference between the incident energy of the earth and the universe, so it is constant and is shown in A of the same figure. horizon 10
If the image of is located somewhere within this linear array sensor element 211, it is possible to determine in which element 211 the boundary lies.

以上述べたように、従来のアナログセンサ゛の出力信号
の絶対値で地球端(地平線)を検出する方式に比較して
、本発明では、検出器自体の温度は問題でないので、検
出器自体の温度を制御する必要がなく、検出器要素をさ
らに細分化すれば、それに応じて精度も向上するという
効果がある。なお精度のそれほど要求されない捕捉領域
センサ22゜23には、温度制御しないアナログセンサ
を使用すればよい。
As mentioned above, compared to the conventional method of detecting the edge of the earth (horizon) using the absolute value of the output signal of an analog sensor, in the present invention, the temperature of the detector itself is not a problem. There is no need to control the temperature, and further subdivision of the detector elements has the effect of increasing accuracy accordingly. Note that analog sensors without temperature control may be used as the capture area sensors 22 and 23, which do not require much accuracy.

このような構成にすることにより第4図に示すように、
X軸に姿勢角をy軸に姿勢誤差信号を取った時、精度の
必要な線形領域d[はりニヤアレイセンサを使用し、精
度のそれほど必要のない捕捉領域eVCは、信号読み出
しの簡単なアナログ型検出器を使用することができる。
With this configuration, as shown in Figure 4,
When the attitude angle is taken on the X axis and the attitude error signal is taken on the y axis, the linear area d that requires accuracy is used. A type detector can be used.

発明の効果 取手のように、本発明は線型領域センサとして複数個の
赤外線検出要素より成るリニアアレイセンサを、捕捉領
域センサとしてアナログセンサを使用した地平線検出装
置で、入射赤外線輻射強度や検出器の温度変化に無関係
に常に高精度にかつ簡単な構成により三軸安定化衛星の
姿勢を検出することができる。
Effects of the Invention Like the handle, the present invention is a horizon detection device that uses a linear array sensor consisting of a plurality of infrared detection elements as a linear area sensor and an analog sensor as a capture area sensor. The attitude of a three-axis stabilized satellite can always be detected with high precision and with a simple configuration regardless of temperature changes.

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

第1図は従来の地平線検出装置の構成を示す概略図、第
2図は本発明による地平線検出装置の構成を示す概念図
、第3図イ9口は第2図の一部拡大図およびその動作説
明図、第4図は本発明による地平線検出装置の動作特性
図である。 10・・・・・・地平線、11・・・・・・地球、12
・・・・・・宇宙、2o・・・・・・検出器、21・・
・・・・リニヤアレイセンサ、22・・・・・・宇宙側
の捕捉領域アナログセンサ、23・・・・・・地球側の
捕捉領域アナログセンサ、211・・・・・・リニヤア
レイセンサの要素、212・・・・・・導電体、24・
・・・・・走査機能素子。 代理人の氏名 弁理士 中 尾 敏 男 ほか1名第1
図 第2図 1θ 第 3yJ lθ
FIG. 1 is a schematic diagram showing the configuration of a conventional horizon detection device, FIG. 2 is a conceptual diagram showing the configuration of a horizon detection device according to the present invention, and FIG. FIG. 4 is an operational characteristic diagram of the horizon detection device according to the present invention. 10...Horizon, 11...Earth, 12
...Space, 2o...Detector, 21...
... Linear array sensor, 22 ... Capture area analog sensor on the space side, 23 ... Capture area analog sensor on the earth side, 211 ... Elements of linear array sensor , 212... conductor, 24.
...Scanning functional element. Name of agent: Patent attorney Toshio Nakao and 1 other person No. 1
Figure 2 1θ 3rd yJ lθ

Claims (1)

【特許請求の範囲】[Claims] 線型領域センサとして複数個の赤外線検出要素を備えた
りニヤアレイセンサを、捕捉領域センサとしてアナログ
センサを用いることを特徴とする地平線検出装置。
A horizon detection device characterized in that it is equipped with a plurality of infrared detection elements or uses a near array sensor as a linear area sensor, and uses an analog sensor as a capture area sensor.
JP57143913A 1982-08-18 1982-08-18 Horizon detector Pending JPS5932600A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57143913A JPS5932600A (en) 1982-08-18 1982-08-18 Horizon detector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57143913A JPS5932600A (en) 1982-08-18 1982-08-18 Horizon detector

Publications (1)

Publication Number Publication Date
JPS5932600A true JPS5932600A (en) 1984-02-22

Family

ID=15349999

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57143913A Pending JPS5932600A (en) 1982-08-18 1982-08-18 Horizon detector

Country Status (1)

Country Link
JP (1) JPS5932600A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63257673A (en) * 1987-04-16 1988-10-25 Oji Paper Co Ltd Ink sheet for electrothermal transfer printer
JPH01104900A (en) * 1987-07-10 1989-04-21 Jujo Paper Co Ltd Highly filled sheet

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63257673A (en) * 1987-04-16 1988-10-25 Oji Paper Co Ltd Ink sheet for electrothermal transfer printer
JPH01104900A (en) * 1987-07-10 1989-04-21 Jujo Paper Co Ltd Highly filled sheet

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