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1.发明授权公开(公告)号：US07577501B2
公开(公告)日：2009-08-18
申请号：US10787644
申请日：2004-02-26
IPC分类号： G06F17/00
CPC分类号： G07C5/085 , G08G5/0013 , G08G5/0039 , G08G5/0052
摘要： Methods and systems for automatically tracking information during flight are disclosed. A method in accordance with one embodiment of the invention includes receiving first information corresponding to a proposed aspect of a flight of the aircraft and including at least one target value. The method can further include automatically receiving second information that includes an actual value corresponding to the at least one target value, as the aircraft executes the flight. The at least one target value and the actual value can be provided together in a common computer-based medium.
摘要翻译： 公开了在飞行中自动跟踪信息的方法和系统。 根据本发明的一个实施例的方法包括接收对应于飞行器的飞行的拟议方面的第一信息并且包括至少一个目标值。 当飞机执行飞行时，该方法还可以包括自动接收包括与至少一个目标值对应的实际值的第二信息。 至少一个目标值和实际值可以一起提供在通用的基于计算机的介质中。
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2.发明授权公开(公告)号：US08027756B2
公开(公告)日：2011-09-27
申请号：US11608064
申请日：2006-12-07
申请人： Robert B. Davis , Daniel J. Boorman , L. Kirk Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
发明人： Robert B. Davis , Daniel J. Boorman , L. Kirk Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
IPC分类号： G05D1/06
CPC分类号： G01C23/00 , G01C21/00 , G01C23/005 , G08G5/0021 , G08G5/025
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。
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3.发明授权公开(公告)号：US08423207B2
公开(公告)日：2013-04-16
申请号：US13218978
申请日：2011-08-26
申请人： Robert B. Davis , Daniel J. Boorman , L. Kirk Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
发明人： Robert B. Davis , Daniel J. Boorman , L. Kirk Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
CPC分类号： G01C23/00 , G01C21/00 , G01C23/005 , G08G5/0021 , G08G5/025
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。
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4.发明申请公开(公告)号：US20110313600A1
公开(公告)日：2011-12-22
申请号：US13218978
申请日：2011-08-26
申请人： Robert B. Davis , Daniel J. Boorman , Kirk L. Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
发明人： Robert B. Davis , Daniel J. Boorman , Kirk L. Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
CPC分类号： G01C23/00 , G01C21/00 , G01C23/005 , G08G5/0021 , G08G5/025
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。
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5.发明申请公开(公告)号：US20080140270A1
公开(公告)日：2008-06-12
申请号：US11608064
申请日：2006-12-07
申请人： Robert B. Davis , Daniel J. Boorman , L. Kirk Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
发明人： Robert B. Davis , Daniel J. Boorman , L. Kirk Gagnon , William L. Goodman , Alan R. Jacobsen , William A. Miller , James E. Mitchell , Victor A. Riley , William F. Royce , William D. Tafs
CPC分类号： G01C23/00 , G01C21/00 , G01C23/005 , G08G5/0021 , G08G5/025
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。
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