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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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