JPS594016U - Satellite attitude control device - Google Patents
Satellite attitude control deviceInfo
- Publication number
- JPS594016U JPS594016U JP9565382U JP9565382U JPS594016U JP S594016 U JPS594016 U JP S594016U JP 9565382 U JP9565382 U JP 9565382U JP 9565382 U JP9565382 U JP 9565382U JP S594016 U JPS594016 U JP S594016U
- Authority
- JP
- Japan
- Prior art keywords
- computer
- satellite
- attitude control
- control device
- satellite attitude
- 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
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は従来の姿勢制御装置を示す図、第２図はこの考
案の一実施例を示す図である。図中１は姿勢センサ系、
２は計算機、３はアクチュエータ系、４はアナログバッ
クアップ回路、５はバックアップ用マイクロプロセッサ
である。なお、図中、同一あるいは相当部分には同一符
号を付して示しである。FIG. 1 is a diagram showing a conventional attitude control device, and FIG. 2 is a diagram showing an embodiment of this invention. 1 in the figure is the attitude sensor system,
2 is a computer, 3 is an actuator system, 4 is an analog backup circuit, and 5 is a backup microprocessor. In the drawings, the same or corresponding parts are designated by the same reference numerals.
Claims (1)
姿勢制御アルゴリズムを演算することを主要機能とした
第１の計算機を搭載した人工衛星の姿勢制御装置におい
て、上記第１の計算機が故障した場合でも人工衛星を安
全な状態に保持する、ため、上記第１の計算機とは別の
第２の計算機をセンサ系とアクチュエータ系との間に設
け、第２の計算機の機能を利用して、第２の計算機自体
に内蔵する第１の計算機と異なるプログラムにより、第
１の計算機が故障した場合でも人工衛星を安全な状態に
保持できるように人工衛星を制御するようにしたことを
特徴とする人工衛星の姿勢制御装置。In a satellite attitude control system equipped with a first computer that is connected to the sensor system and actuator system and whose main function is to calculate the attitude control algorithm of the satellite, even if the first computer fails, the satellite In order to maintain the computer in a safe state, a second computer separate from the first computer is provided between the sensor system and the actuator system, and the function of the second computer is used to control the operation of the second computer. An attitude of an artificial satellite characterized in that the artificial satellite is controlled by a program different from the first computer built into itself so that the satellite can be maintained in a safe state even if the first computer fails. Control device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9565382U JPS594016U (en) | 1982-06-25 | 1982-06-25 | Satellite attitude control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9565382U JPS594016U (en) | 1982-06-25 | 1982-06-25 | Satellite attitude control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS594016U true JPS594016U (en) | 1984-01-11 |
Family
ID=30228329
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9565382U Pending JPS594016U (en) | 1982-06-25 | 1982-06-25 | Satellite attitude control device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS594016U (en) |
-
1982
- 1982-06-25 JP JP9565382U patent/JPS594016U/en active Pending
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