发明名称 CONTROL AIRCRAFT GUIDANCE SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a control aircraft guidance system which enables safe and sure guidance for aircraft proceeding into an apron zone, even when the amount of air services is large. SOLUTION: The control aircraft guidance system consists of at least a pair of measuring methods 13, a storage method 11b, position specifying method 11c1, and outputting method 9. The measurement methods 13 measure relative position between an aircraft 1 and a parking position of the aircraft. The storage method 11b stores parking zone figure including more than one parking positions in an airport. The position-specifying method 11c1 specifies the position of the aircraft on the parking zone picture, on the basis of the relative position of the aircraft 1 measured by the parking zone figure and measurement method 13. The output method 9 outputs information related to guidance for the aircraft 1, on the basis of the position of the aircraft 1 specified by the position-specifying method 11c1 for the aircraft. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005259151(A) 申请公布日期 2005.09.22
申请号 JP20050080282 申请日期 2005.03.18
申请人 TOSHIBA CORP 发明人 SATO TAKAKAZU
分类号 B64F1/36;G08G5/06;(IPC1-7):G08G5/06 主分类号 B64F1/36
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