首页> 外国专利> 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

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

机译:飞机导航系统,具有飞行管理系统,该飞行管理系统确定与估计速度有关的飞行参数的估计值以扩展高升力设备,并且导航显示器显示相对于估计值的符号

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.
机译:该系统具有飞行管理系统,该飞行管理系统用于计算飞机(14)的估计飞行路径(12)并且用于确定例如飞行参数的飞行参数的估计值。高度和速度,对应于飞机高升力装置伸展的估计速度。主飞行显示器显示飞行路线,导航显示器显示相对于参数估计值的符号(18、20)。还包括以下方面的独立权利要求:(A)具有导航系统的飞机(B)用于控制航空器的导航系统的方法。

著录项

相似文献

  • 专利
  • 外文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号