JPH0239999U - - Google Patents

Info

Publication number
JPH0239999U
JPH0239999U JP11856688U JP11856688U JPH0239999U JP H0239999 U JPH0239999 U JP H0239999U JP 11856688 U JP11856688 U JP 11856688U JP 11856688 U JP11856688 U JP 11856688U JP H0239999 U JPH0239999 U JP H0239999U
Authority
JP
Japan
Prior art keywords
accelerometer
angular velocity
synchronization
satellite
nutrition
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
JP11856688U
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 JP11856688U priority Critical patent/JPH0239999U/ja
Publication of JPH0239999U publication Critical patent/JPH0239999U/ja
Pending legal-status Critical Current

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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図は本考案の一実施例の構成図、第2図は
本実施例の原理説明図、第2図のAは第2図のC
MG2の拡大図である。 1……加速度計、2……シングル ジンバル
コントロール モーメント ジヤイロ(CMG)
、3……駆動装置、4……ロータ、5……ジンバ
ル、6……モーメンタム・ホイール、7……衛星
本体、8……角速度ベクトル、9……方向、10
……リアクシヨントルク、11……CMGの発生
トルク。
Figure 1 is a configuration diagram of an embodiment of the present invention, Figure 2 is a diagram explaining the principle of this embodiment, and A in Figure 2 is C in Figure 2.
It is an enlarged view of MG2. 1...accelerometer, 2...single gimbal
Control moment gyroscope (CMG)
, 3... Drive device, 4... Rotor, 5... Gimbal, 6... Momentum wheel, 7... Satellite body, 8... Angular velocity vector, 9... Direction, 10
...Reaction torque, 11... CMG generated torque.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 衛星本体のニユーテーシヨンによる角速度の方
向と同期とを検出する加速度計と、前記加速度計
の検出信号の角速度と、同一方向と同期に対応す
る駆動力を出力する駆動装置と、前記駆動装置の
出力により回転するジンバル機構を有するコント
ロール モーメント ジヤイロとを備えたことを
特徴とする衛星のニユーテーシヨンダンピング装
置。
an accelerometer that detects the direction and synchronization of the angular velocity due to the nutrition of the satellite body; a drive device that outputs a driving force corresponding to the same direction and synchronization as the angular velocity of the detection signal of the accelerometer; A satellite news damping device characterized by comprising a control moment gyroscope having a gimbal mechanism that rotates based on output.
JP11856688U 1988-09-09 1988-09-09 Pending JPH0239999U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11856688U JPH0239999U (en) 1988-09-09 1988-09-09

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11856688U JPH0239999U (en) 1988-09-09 1988-09-09

Publications (1)

Publication Number Publication Date
JPH0239999U true JPH0239999U (en) 1990-03-19

Family

ID=31363021

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11856688U Pending JPH0239999U (en) 1988-09-09 1988-09-09

Country Status (1)

Country Link
JP (1) JPH0239999U (en)

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