发明名称 Satellite position and path regulation method uses reflection of electromagnetic radiation by adjustable reflection surface mounted on satellite for providing correction drive pulse
摘要 The position and path regulation method uses at least one reflection surface (3) mounted on the satellite (1), with a radiation reflection characteristics which is matched to an earth electromagnetic radiation source, e.g. a laser, for providing a position or path correction drive pulse via the radiation reflection.
申请公布号 DE19848737(A1) 申请公布日期 2000.04.27
申请号 DE19981048737 申请日期 1998.10.22
申请人 DAIMLERCHRYSLER AEROSPACE AKTIENGESELLSCHAFT 发明人 MANG, VOLKER;ZIER, MANFRED;WEBER, KARL-HEINZ
分类号 B64G1/24;B64G1/32;B64G1/40;B64G1/44;G05D1/08;(IPC1-7):G05D1/08;H01L31/00 主分类号 B64G1/24
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