发明名称 Aircraft navigation system, has flight management system determining estimated value of flight parameter related to estimated speed for extension of high-lift devices, and navigation display displaying symbols relative to estimated value
摘要 The system has a flight management system for calculating an estimated flight path (12) for an aircraft (14) and for determining an estimated value of a flight parameter e.g. altitude and speed, corresponding to an estimated speed for extension of high-lift devices of the aircraft. A primary flight display displays the flight line, and a navigation display displays symbols (18, 20) relative to the estimated value of the parameter. Independent claims are also included for the following: (A) an aircraft having a navigation system (B) a method for controlling a navigation system of an aircraft.
申请公布号 FR2881221(A1) 申请公布日期 2006.07.28
申请号 FR20050008212 申请日期 2005.08.01
申请人 AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE 发明人 FERRO DANIEL;VAN BOVEN MACHIEL
分类号 G01C23/00;B64C13/18;B64D43/00;G05D1/06 主分类号 G01C23/00
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