INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT
    1.
    发明申请
    INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT 有权
    综合方法导航系统,方法和计算机程序产品

    公开(公告)号:US20110313600A1

    公开(公告)日:2011-12-22

    申请号:US13218978

    申请日:2011-08-26

    IPC分类号: G01C23/00 G05D1/00

    摘要: Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.

    摘要翻译: 提供了系统,计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。 基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系,飞行模式和方面以及相关程序,相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示 在最终进场段期间从预定义的飞行路径到跑道和着陆期间。 例如,增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记,以警告飞行员和飞行机组成员FMC已经从用于RNAV(LNAV / VNAV)飞行程序的NPS显示器转换 到非精确(非xLS)方法和/或着陆的增强型IAN显示。

    Integrated approach navigation system, method, and computer program product
    2.
    发明授权
    Integrated approach navigation system, method, and computer program product 有权
    综合导航系统,方法和计算机程序产品

    公开(公告)号:US08027756B2

    公开(公告)日:2011-09-27

    申请号:US11608064

    申请日:2006-12-07

    IPC分类号: G05D1/06

    摘要: Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.

    摘要翻译: 提供了系统,计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。 基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系,飞行模式和方面以及相关程序,相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示 在最终进场段期间从预定义的飞行路径到跑道和着陆期间。 例如,增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记,以警告飞行员和飞行机组成员FMC已经从用于RNAV(LNAV / VNAV)飞行程序的NPS显示器转换 到非精确(非xLS)方法和/或着陆的增强型IAN显示。

    Integrated approach navigation system, method, and computer program product
    3.
    发明授权
    Integrated approach navigation system, method, and computer program product 有权
    综合导航系统,方法和计算机程序产品

    公开(公告)号:US08423207B2

    公开(公告)日:2013-04-16

    申请号:US13218978

    申请日:2011-08-26

    摘要: Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.

    摘要翻译: 提供了系统,计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。 基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系,飞行模式和方面以及相关程序,相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示 在最终进场段期间从预定义的飞行路径到跑道和着陆期间。 例如,增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记,以警告飞行员和飞行机组成员FMC已经从用于RNAV(LNAV / VNAV)飞行程序的NPS显示器转换 到非精确(非xLS)方法和/或着陆的增强型IAN显示。

    INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT
    4.
    发明申请
    INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT 有权
    综合方法导航系统,方法和计算机程序产品

    公开(公告)号:US20080140270A1

    公开(公告)日:2008-06-12

    申请号:US11608064

    申请日:2006-12-07

    IPC分类号: G01C21/00 G05D1/00

    摘要: Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.

    摘要翻译: 提供了系统,计算机程序产品以及在最终进场段到跑道和非精确飞行模式着陆期间显示导航性能的飞行路径偏差信息的方法。 基于导航性能的飞行路径偏差信息的改进图形描述为飞行员和飞行机组成员提供了ANP和RNP之间的动态关系,飞行模式和方面以及相关程序,相交飞行路径以及当前实际飞行路径偏差的清晰简明的显示 在最终进场段期间从预定义的飞行路径到跑道和着陆期间。 例如,增强的IAN显示器可以包括NPS型偏差标度以显示RNP / ANP关系和预定的RNP标记,以警告飞行员和飞行机组成员FMC已经从用于RNAV(LNAV / VNAV)飞行程序的NPS显示器转换 到非精确(非xLS)方法和/或着陆的增强型IAN显示。