发明名称 METHOD AND SYSTEM FOR ASSISTING FLIGHT CONTROL OF A LOW-FLYING AIRCRAFT
摘要 <p>A system determines a limit angle of climb corresponding to a climb angle of an aircraft for flying over the ground along an avoidance path and displays a characteristic sign representing the limit angle of climb on a display screen.</p>
申请公布号 EP1891618(A2) 申请公布日期 2008.02.27
申请号 EP20060764769 申请日期 2006.06.12
申请人 AIRBUS FRANCE 发明人 BOUCHET, CHRISTOPHE;DEMORTIER, JEAN-PIERRE;ARTINI, FRANCK
分类号 G08G5/04;B64D43/00;G01C23/00 主分类号 G08G5/04
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