JPH0383200U - - Google Patents
Info
- Publication number
- JPH0383200U JPH0383200U JP14559689U JP14559689U JPH0383200U JP H0383200 U JPH0383200 U JP H0383200U JP 14559689 U JP14559689 U JP 14559689U JP 14559689 U JP14559689 U JP 14559689U JP H0383200 U JPH0383200 U JP H0383200U
- Authority
- JP
- Japan
- Prior art keywords
- attitude
- control device
- orbit
- gyroscope
- processing unit
- 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
Links
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図はこの考案の一実施例を示す図。第２図
は第１図の分割処理装置におけるデータの分割を
示した図である。１……蓄積外乱データ、２……
分割処理装置、３……ジヤイロ、４……姿勢決定
部、５……姿勢制御部、６……リアクシヨンホイ
ール、７……磁気制御装置である。なお、各図中
同一符号は同一又は相当部分を示す。
FIG. 1 is a diagram showing an embodiment of this invention. FIG. 2 is a diagram showing the division of data in the division processing device of FIG. 1. 1... Accumulated disturbance data, 2...
3... Gyro, 4... Attitude determining section, 5... Attitude control section, 6... Reaction wheel, 7... Magnetic control device. Note that the same reference numerals in each figure indicate the same or corresponding parts.
Claims (1)
気制御装置を用いて行う長楕円軌道地球周回型人
工衛星の姿勢制御装置において、ジヤイロと、上
記ジヤイロの出力信号により、衛星の姿勢情報を
計算する姿勢決定部と、軌道一周における蓄積外
乱の永年項のデータと、上記永年項のデータを軌
道位置において分割する分割処理部と、上記姿勢
決定部と上記分割処理部からの信号によつて、リ
アクシヨンホイールと磁気制御装置を駆動する姿
勢制御部とを有することを特徴とする人工衛星の
姿勢制御装置。 In an attitude control device for an artificial satellite orbiting the Earth in an elongated elliptical orbit that unloads a reaction wheel using a magnetic control device, the attitude determining unit calculates attitude information of the satellite based on a gyroscope and an output signal of the gyroscope; The reaction wheel and magnetic control are performed using the secular term data of accumulated disturbances during one orbit, a division processing unit that divides the secular term data at orbit positions, and signals from the attitude determination unit and the division processing unit. An attitude control device for an artificial satellite, comprising an attitude control section that drives the device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14559689U JPH0383200U (en) | 1989-12-18 | 1989-12-18 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14559689U JPH0383200U (en) | 1989-12-18 | 1989-12-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0383200U true JPH0383200U (en) | 1991-08-23 |
Family
ID=31692224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14559689U Pending JPH0383200U (en) | 1989-12-18 | 1989-12-18 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0383200U (en) |
-
1989
- 1989-12-18 JP JP14559689U patent/JPH0383200U/ja active Pending
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