JPS6330300U - - Google Patents
Info
- Publication number
- JPS6330300U JPS6330300U JP12486886U JP12486886U JPS6330300U JP S6330300 U JPS6330300 U JP S6330300U JP 12486886 U JP12486886 U JP 12486886U JP 12486886 U JP12486886 U JP 12486886U JP S6330300 U JPS6330300 U JP S6330300U
- Authority
- JP
- Japan
- Prior art keywords
- output
- magnetic torque
- converter
- detection circuit
- current detection
- 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
Landscapes
- Radio Relay Systems (AREA)
Description
第１図はこの考案の実施例を示すブロツク図、
第２図は従来の人工衛星搭載用磁気トルク制御装
置を示すブロツク図である。
図において、１は外部入力制御信号、２はＤＣ
／ＤＣコンバータ、３は電力制御回路、４は磁気
トルク発生器、５はＤＣ／ＤＣコンバータ基準電
圧、６は電流検出回路、７は誤差増幅器である。
なお、各図中同一符号は同一または相当部分を示
す。
Figure 1 is a block diagram showing an embodiment of this invention.
FIG. 2 is a block diagram showing a conventional magnetic torque control device mounted on an artificial satellite. In the figure, 1 is an external input control signal, 2 is a DC
3 is a power control circuit, 4 is a magnetic torque generator, 5 is a DC/DC converter reference voltage, 6 is a current detection circuit, and 7 is an error amplifier.
Note that the same reference numerals in each figure indicate the same or corresponding parts.
Claims (1)
検出回路と、この電流検出回路の出力と外部入力
制御信号との誤差を増幅する誤差増幅器と、この
誤差増幅器の出力に応じて出力電圧が変化するＤ
Ｃ／ＤＣコンバータとを備え、前記ＤＣ／ＤＣコ
ンバータの出力で直接人工衛星搭載用磁気トルク
発生器を駆動することを特徴とする人工衛星搭載
用磁気トルク制御装置。 A current detection circuit that detects the current flowing through the magnetic torque generator, an error amplifier that amplifies the error between the output of this current detection circuit and an external input control signal, and a D whose output voltage changes according to the output of this error amplifier.
What is claimed is: 1. A magnetic torque control device mounted on an artificial satellite, comprising: a C/DC converter, and directly drives a magnetic torque generator mounted on the artificial satellite with the output of the DC/DC converter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12486886U JPS6330300U (en) | 1986-08-14 | 1986-08-14 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12486886U JPS6330300U (en) | 1986-08-14 | 1986-08-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6330300U true JPS6330300U (en) | 1988-02-27 |
Family
ID=31017261
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12486886U Pending JPS6330300U (en) | 1986-08-14 | 1986-08-14 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6330300U (en) |
-
1986
- 1986-08-14 JP JP12486886U patent/JPS6330300U/ja active Pending
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