发明名称 TRACKING SYSTEM FOR SPACE AIRFRAME
摘要 PURPOSE:To decrease the amount of calculation by forecasting the moving direction of a sattelite by extrapolation without deciding on a track element, etc. CONSTITUTION:The radio wave output of an antenna 1 for tracking is connected to a tracking receiver 2, whose output signal is supplied to a control circuit 4 for EL (elevation) control and a control circuit 5 for AZ (azimuth) control. Further, the EL angle and AZ angle of displacement of machine systems 10 and 11 are detected by angle detectors 12 and 13, whose detection outputs are supplied to a zenith tracking device 15. Its output is supplied as input control signals to said control circuits 4 and 5.
申请公布号 JPS5886472(A) 申请公布日期 1983.05.24
申请号 JP19810184912 申请日期 1981.11.17
申请人 NIPPON DENKI KK 发明人 SHIMIZU TAKASHI
分类号 B64G3/00;G01S13/68;G05D1/12 主分类号 B64G3/00
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