JPH0263299U - - Google Patents

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Publication number
JPH0263299U
JPH0263299U JP14352888U JP14352888U JPH0263299U JP H0263299 U JPH0263299 U JP H0263299U JP 14352888 U JP14352888 U JP 14352888U JP 14352888 U JP14352888 U JP 14352888U JP H0263299 U JPH0263299 U JP H0263299U
Authority
JP
Japan
Prior art keywords
attitude
rotating wheel
satellite
torque
rotation speed
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
JP14352888U
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 JP14352888U priority Critical patent/JPH0263299U/ja
Publication of JPH0263299U publication Critical patent/JPH0263299U/ja
Pending legal-status Critical Current

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  • 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
は従来の磁気姿勢制御装置の一例を示した図であ
る。 図中、1は制御器、2は磁気コイル制御信号、
3は磁気コイル、4は発生磁気、5は地磁気、6
は制御トルク、7は衛星ダイナミクス、8は外乱
トルク、9は入力トルク、10は磁気浮上支持型
回転輪、11は姿勢センサ、12は姿勢信号、1
3は回転輪駆動器、14は回転輪駆動信号、15
は検出器、16は回転数信号、17は地上局、1
8は磁気制御コマンドである。なお、各図中同一
符号は同一または相当部分を示す。
FIG. 1 is a diagram showing an embodiment of this invention, and FIG. 2 is a diagram showing an example of a conventional magnetic attitude control device. In the figure, 1 is a controller, 2 is a magnetic coil control signal,
3 is a magnetic coil, 4 is generated magnetism, 5 is earth's magnetism, 6
is a control torque, 7 is a satellite dynamics, 8 is a disturbance torque, 9 is an input torque, 10 is a magnetic levitation supported rotating wheel, 11 is an attitude sensor, 12 is an attitude signal, 1
3 is a rotary wheel drive device, 14 is a rotary wheel drive signal, 15
is a detector, 16 is a rotational speed signal, 17 is a ground station, 1
8 is a magnetic control command. Note that the same reference numerals in each figure 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] 人工衛星に外乱トルクが作用し、人工衛星の一
定面が地球に向かなくなるように変化したとき、
人工衛星の姿勢の変化を検出し、姿勢の変化に比
例した姿勢信号を出力する姿勢センサと、姿勢信
号の変化に比例した回転輪駆動信号を磁気浮上支
持型回転輪に伝達する回転輪駆動器と、磁気浮上
支持型回転輪の回転数を検出し、回転数に比例し
た回転数信号を制御器に伝達する検出器と、回転
数信号と外乱トルクを打消すトルクコマンドを発
生する地上局からの磁気制御コマンドの大きさを
比較し、両信号の差に比例した磁気コイル制御信
号を磁気コイルに出力する制御器と、磁気コイル
制御信号に比例して磁気コイルが発生する発生磁
気を地磁気に作用させることによつて起こす制御
トルクを外乱トルクから差し引くことによつて、
入力トルクを磁気浮上支持型回転輪に伝達する衛
星ダイナミクスとを備え、磁気浮上支持型回転輪
に入力トルクを加えることによつて磁気浮上支持
型回転輪の持つ角運動量を制御し、人工衛星の姿
勢を、地球に対して人工衛星の一定面が常に向く
ように制御することを特徴とする人工衛星の磁気
姿勢制御装置。
When a disturbance torque acts on an artificial satellite and the certain side of the artificial satellite changes so that it no longer faces the earth,
An attitude sensor that detects changes in the satellite's attitude and outputs an attitude signal proportional to the change in attitude, and a rotating wheel driver that transmits a rotating wheel drive signal proportional to the change in attitude signal to the magnetically supported rotating wheel. , a detector that detects the rotation speed of the magnetically supported rotating wheel and transmits a rotation speed signal proportional to the rotation speed to the controller, and a ground station that generates a torque command to cancel the rotation speed signal and disturbance torque. A controller that compares the magnitude of magnetic control commands and outputs a magnetic coil control signal proportional to the difference between the two signals to the magnetic coil, and a controller that outputs the generated magnetism generated by the magnetic coil in proportion to the magnetic coil control signal to the earth's magnetism. By subtracting the control torque caused by the action from the disturbance torque,
It is equipped with satellite dynamics that transmits input torque to the magnetically supported rotating wheel, and controls the angular momentum of the magnetically supported rotating wheel by applying input torque to the magnetically supported rotating wheel. A magnetic attitude control device for an artificial satellite, which controls the attitude of the satellite so that a certain side of the satellite always faces the earth.
JP14352888U 1988-11-02 1988-11-02 Pending JPH0263299U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14352888U JPH0263299U (en) 1988-11-02 1988-11-02

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14352888U JPH0263299U (en) 1988-11-02 1988-11-02

Publications (1)

Publication Number Publication Date
JPH0263299U true JPH0263299U (en) 1990-05-11

Family

ID=31410428

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14352888U Pending JPH0263299U (en) 1988-11-02 1988-11-02

Country Status (1)

Country Link
JP (1) JPH0263299U (en)

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