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.
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
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