JPS6151300U - - Google Patents

Info

Publication number
JPS6151300U
JPS6151300U JP13685084U JP13685084U JPS6151300U JP S6151300 U JPS6151300 U JP S6151300U JP 13685084 U JP13685084 U JP 13685084U JP 13685084 U JP13685084 U JP 13685084U JP S6151300 U JPS6151300 U JP S6151300U
Authority
JP
Japan
Prior art keywords
earth
signal
attitude
artificial satellite
control
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
JP13685084U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP13685084U priority Critical patent/JPS6151300U/ja
Publication of JPS6151300U publication Critical patent/JPS6151300U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Description

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

第1図は従来の地球センサの干渉除去機能を示
す機能ブロツク図、第2図は姿勢制御電子回路部
を通さない場合の地球角信号を示す図、第3図は
姿勢制御電子回路部を通し地球角を零度に制御し
ている時の地球角信号を示す図、第4図はこの考
案の一実施例を示す機能ブロツク図、第5図はこ
の考案を適用した場合で、かつ姿勢制御電子回路
部を通さない場合の地球角信号を示す図、第6図
はこの考案を適用した場合で、かつ姿勢制御電子
回路部を通し地球角を零度に制御している時の地
球角信号を示す図であり、図において、1及び1
aは地球像、2a,2b,2c及び2dはアース
デイテクタ、3a,3b,3c及び3dはサンデ
イテクタ、4は地球角の検出軸、5a及び5bは
差動アンプ、6は干渉検出部、7はデイテクタペ
ア選択部、8は地球角信号、9は姿勢制御電子回
路部、10はアクチユエータ、11は信号選択部
、12はフイルタである。なお、図中同一符号は
同一または相当部分を示す。
Figure 1 is a functional block diagram showing the interference removal function of a conventional earth sensor, Figure 2 is a diagram showing the earth angle signal when it is not passed through the attitude control electronic circuit, and Figure 3 is a diagram showing the earth angle signal when it is passed through the attitude control electronic circuit. A diagram showing the earth angle signal when the earth angle is controlled to zero degrees, Figure 4 is a functional block diagram showing one embodiment of this invention, and Figure 5 is a diagram showing the case where this invention is applied, and the attitude control electronics. Figure 6 shows the earth angle signal when the circuit is not passed through it. Figure 6 shows the earth angle signal when this idea is applied and the earth angle is controlled to zero degrees through the attitude control electronic circuit. In the figure, 1 and 1
a is an earth image, 2a, 2b, 2c and 2d are earth detectors, 3a, 3b, 3c and 3d are sun detectors, 4 is an earth angle detection axis, 5a and 5b are differential amplifiers, 6 is an interference detection unit, and 7 is an A detector pair selection section, 8 is an earth angle signal, 9 is an attitude control electronic circuit section, 10 is an actuator, 11 is a signal selection section, and 12 is a filter. Note that the same reference numerals in the figures indicate the same or corresponding parts.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 人工衛星に搭載され、人工衛星の地球に対する
地球角を検出する地球センサと、上記地球センサ
からの干渉検出信号を受け地球角信号の出力を切
換える信号選択部と、上記信号選択部を経由して
出力される2本の地球角信号ラインの内の一方に
接続されたフイルタと、フイルタ出力、又は、フ
イルタを通さない地球角信号を受けて、人工衛星
の姿勢を制御する制御信号を出力する姿勢制御電
子回路部と、姿勢制御電子回路部からの制御信号
を受け人工衛星の姿勢を変えるアクチユエータを
備えたことを特徴とする地球センサの太陽干渉除
去装置。
an earth sensor mounted on the artificial satellite that detects the earth angle of the artificial satellite with respect to the earth; a signal selection section that receives an interference detection signal from the earth sensor and switches the output of the earth angle signal; A filter connected to one of the two output earth angle signal lines, and an attitude that receives the filter output or the earth angle signal that does not pass through the filter and outputs a control signal to control the attitude of the artificial satellite. A solar interference removal device for an earth sensor, comprising a control electronic circuit section and an actuator that changes the attitude of an artificial satellite in response to a control signal from the attitude control electronic circuit section.
JP13685084U 1984-09-10 1984-09-10 Pending JPS6151300U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13685084U JPS6151300U (en) 1984-09-10 1984-09-10

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13685084U JPS6151300U (en) 1984-09-10 1984-09-10

Publications (1)

Publication Number Publication Date
JPS6151300U true JPS6151300U (en) 1986-04-07

Family

ID=30695283

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13685084U Pending JPS6151300U (en) 1984-09-10 1984-09-10

Country Status (1)

Country Link
JP (1) JPS6151300U (en)

Similar Documents

Publication Publication Date Title
EP0203396A3 (en) Electronic turn signal cancellation apparatus
JPS6151300U (en)
JPS6034098U (en) earth sensor
JPH01152900U (en)
JP2798938B2 (en) 3-axis attitude control device
JPS58187811U (en) Satellite attitude control device
JPS60168700U (en) sun sensor
JPH0298097U (en)
JPS6146800A (en) Earth sensor
JPS6172618U (en)
JPH0235020U (en)
JPS6339100U (en)
JPS6144399U (en) Satellite magnetic attitude control device
JPS5871000U (en) earth sensor
JPS6230105U (en)
JPH0457716U (en)
JPH0299099U (en)
JPS63101813U (en)
JPS61100650U (en)
JPS62167799U (en)
JPS60100300U (en) spin sun sensor
JPH0316021U (en)
JPH0230008U (en)
JPS61128119A (en) Posture sensor of moving body
Diedrickson et al. An autonomous system for mitigating Earth radiance errors