发明名称 |
Inertial sensor for the mounting and checking of an inertial reference in a satellite |
摘要 |
An inertial sensor includes an inertial reference for determining the attitude and position of a satellite or satellite parts. A test mass is situated in a space which is essentially free of electric and magnetic fields and is enclosed by a housing, and optical measuring sections are set up between reference elements on the housing and on the test mass, for determining the attitude and/or position of the test mass relative to the reference elements on the housing. A measuring arrangement is situated outside the housing for the optical measuring sections. The optical measuring sections are constructed as optical interferometric measuring elements; and the attitude and position of the test mass can be adjusted by means of the pressures of light exerted on the optical interferometric measuring sections upon the test mass.
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申请公布号 |
US6606908(B2) |
申请公布日期 |
2003.08.19 |
申请号 |
US20010892782 |
申请日期 |
2001.06.28 |
申请人 |
ASTRIUM GMBH |
发明人 |
JOHANN ULRICH;JOERCK HARTMUT |
分类号 |
B64G1/10;B64G1/24;B64G1/28;B64G1/32;B64G1/36;G01P15/08;G01P15/13;(IPC1-7):G01P15/08;G06F7/00 |
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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