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.
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
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