| 发明名称 |
Method for maintaining the solar orientation of a satellite |
| 摘要 |
The solar orientation of a satellite which is preferably stabilised in three axes is maintained in the earth's shadow in that it is aligned with an axis parallel to the direction of the incident solar radiation before being immersed in the earth's shadows, and is driven around this axis. <IMAGE>
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| 申请公布号 |
DE3214384(A1) |
申请公布日期 |
1983.10.27 |
| 申请号 |
DE19823214384 |
申请日期 |
1982.04.20 |
| 申请人 |
MITSUBISHI ELECTRIC CORP.;MESSERSCHMITT-BOELKOW-BLOHM GMBH |
发明人 |
SCHEIT,ARNOLD,DIPL.-PHYS.;OKADA,KENJI |
| 分类号 |
B64G1/24;B64G1/28;B64G1/36;G05D1/08;(IPC1-7):G05D1/08 |
主分类号 |
B64G1/24 |
| 代理机构 |
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代理人 |
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| 地址 |
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