发明名称 |
High precision positioning system for orbiting satellite controls measuring apparatus able to generate by itself signals needed for inertial orientation |
摘要 |
The positioning system controls a measuring apparatus (1) that can move freely in a space (3) inside the satellite structure (2). The device generates by itself reference signals needed for inertial orientation and orients itself with a first positioning apparatus (7) toward a goal. The satellite structure follows the movement of the measuring apparatus to screen out parasitic forces and moments.
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申请公布号 |
DE19921390(A1) |
申请公布日期 |
2000.11.30 |
申请号 |
DE19991021390 |
申请日期 |
1999.05.10 |
申请人 |
DAIMLERCHRYSLER AG |
发明人 |
JOERCK, HARTMUT |
分类号 |
B64G1/10;B64G1/24;B64G1/32;B64G1/36;B64G1/66;(IPC1-7):B64G1/24;G05D1/10 |
主分类号 |
B64G1/10 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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