JPH0391898U - - Google Patents

Info

Publication number
JPH0391898U
JPH0391898U JP83990U JP83990U JPH0391898U JP H0391898 U JPH0391898 U JP H0391898U JP 83990 U JP83990 U JP 83990U JP 83990 U JP83990 U JP 83990U JP H0391898 U JPH0391898 U JP H0391898U
Authority
JP
Japan
Prior art keywords
satellite
integrator
accelerometer
output
orbit 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
JP83990U
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 JP83990U priority Critical patent/JPH0391898U/ja
Publication of JPH0391898U publication Critical patent/JPH0391898U/ja
Pending legal-status Critical Current

Links

Landscapes

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

Description

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

第1図はこの考案の一実施例を示す図、第2図
a〜cは第1図に示すコントローラの動作を示す
図、第3図は従来の軌道制御装置の動作を示す図
である。1……加速度計、2……積算器、3……
コントローラ、4……軌道制御用スラスタ、5…
…衛生ダイナミクスである。
FIG. 1 is a diagram showing an embodiment of this invention, FIGS. 2 a to 2 c are diagrams showing the operation of the controller shown in FIG. 1, and FIG. 3 is a diagram showing the operation of a conventional orbit control device. 1...Accelerometer, 2...Integrator, 3...
Controller, 4... Orbit control thruster, 5...
…It is a hygiene dynamic.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 人工衛星の一軸方向の加速度を検出する加速度
計と、上記加速度計の出力を積算し、上記人工衛
星に加えられた速度増分を出力する積算器と、上
記積算器からの出力によつて、上記人工衛星に取
り付けられた軌道制御用スラスタをオンオフ制御
するコントローラとを備えたことを特徴とする人
工衛星の軌道制御装置。
an accelerometer that detects acceleration in a uniaxial direction of the satellite; an integrator that integrates the output of the accelerometer and outputs a velocity increment applied to the satellite; and an output from the integrator. An orbit control device for an artificial satellite, comprising: a controller that controls on/off an orbit control thruster attached to an artificial satellite.
JP83990U 1990-01-09 1990-01-09 Pending JPH0391898U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP83990U JPH0391898U (en) 1990-01-09 1990-01-09

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP83990U JPH0391898U (en) 1990-01-09 1990-01-09

Publications (1)

Publication Number Publication Date
JPH0391898U true JPH0391898U (en) 1991-09-19

Family

ID=31504776

Family Applications (1)

Application Number Title Priority Date Filing Date
JP83990U Pending JPH0391898U (en) 1990-01-09 1990-01-09

Country Status (1)

Country Link
JP (1) JPH0391898U (en)

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