<p>The guidance system (1) comprises means (2, 6) for generating an alphanumeric identification characteristic, making it possible to identify a data item which must be used for a selected guidance mode of the aircraft, and display means (10) which automatically show this alphanumeric identification characteristic on a display screen (12).</p>
申请公布号
WO2007110503(A1)
申请公布日期
2007.10.04
申请号
WO2007FR00516
申请日期
2007.03.26
申请人
AIRBUS FRANCE;MARKITON, VINCENT;PEYRUCAIN, ERIC;BERTIN, LIONEL;DE MENORVAL, JEAN-LOUIS
