发明名称 Landing guide installation on path of landing aircraft
摘要 The aircraft (12) has two sources of light on-board, with the first source (14,16) is aimed to be seen directly at the landing site and a second source (14,18) shines vertically downward. At the landing site a camera (22) is aimed at the correct direction of approach for aircraft.The images produced by the camera (22) are processed (24,26,30) to allow if necessary for the movement of the landing site, if it were an aircraft carrier, and to produce a picture showing the actual position of the aircraft relative to a correct position. Necessary corrections are signalled to the pilot (28).
申请公布号 FR2727082(A1) 申请公布日期 1996.05.24
申请号 FR19940013945 申请日期 1994.11.22
申请人 CHAUTHAI LUC 发明人
分类号 B64F1/18;G05D1/06;(IPC1-7):B64F1/18;G01C21/00 主分类号 B64F1/18
代理机构 代理人
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