发明名称 Flight guidance system for aircraft
摘要 The radar control system 1000 has a control unit 1060 that receives inputs from an inertial navigation unit 1030, a GPS system 1020 and a flight path computer 3010. Output is provided to the auto pilot 1070 and the pilot display 1040. The communication link is provided with a synthetic aperture unit 2000 and this has inputs from microwave antenna 2021,2022 that are processed 2070 to provide a precise two dimensional model of the area being flown over.
申请公布号 DE19703736(A1) 申请公布日期 1997.11.06
申请号 DE19971003736 申请日期 1997.02.01
申请人 MOREIRA, JOAO R., DR.-ING., 82110 GERMERING, DE 发明人 MOREIRA, JOAO R., DR.-ING., 82110 GERMERING, DE
分类号 G01S7/00;G01S7/40;G01S13/86;G01S13/90;(IPC1-7):G01S13/89;G05D1/10;G08C17/02;G08G5/00 主分类号 G01S7/00
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