发明名称 Approach Phase Monitoring System for an Aircraft
摘要 The invention relates to a monitoring system dedicated to the landing of an aircraft including means of receiving navigation data, means of receiving a plurality of landing area monitoring information, and display means representing, by various symbols, the landing area and the monitoring information, including means of determining a plurality of successive approach phases constituting the landing procedure and of signalling the current approach phase, means of calculating a plurality of cartographic scale factors of the landing area, and means of selecting monitoring information to be displayed for each approach phase. The display means represent the landing area according to a changing cartographic scale factor and the selected monitoring information by symbols that also change, the cartographic scale factor and the symbols changing automatically according to the current approach phase.
申请公布号 US2011246003(A1) 申请公布日期 2011.10.06
申请号 US20100898559 申请日期 2010.10.05
申请人 THALES 发明人 LAFON STEPHANIE;DUBOURG BERNARD;MICHEL FRANCOIS
分类号 G08G5/02;G06F19/00 主分类号 G08G5/02
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