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1. 发明申请

US20100305786A1 METHOD AND SYSTEM FOR APPROACH DECISION DISPLAY 有权
标题翻译：方法决策显示方法与系统
公开(公告)号：US20100305786A1
公开(公告)日：2010-12-02
申请号：US12474122
申请日：2009-05-28
申请人： DANIEL J. BOORMAN
发明人： DANIEL J. BOORMAN
IPC分类号： G01C23/00 , G06F19/00 , G06G7/76
CPC分类号： G08G5/0021 , G08G5/025
摘要： Approach Decision Display and associated methods and systems are disclosed. A method and system in accordance to one embodiment of the disclosure includes a display of operationally-relevant information for final approach and landing on a cockpit graphical display. Approach Decision Display System (ADDS) provides, in a graphical display, dynamic decision parameters as a function of the health of required equipment for the selected approach and the aircraft's ability to execute the approach and landing.
摘要翻译：方法决策显示和相关方法和系统被公开。根据本公开的一个实施例的方法和系统包括用于最终进近和在驾驶舱图形显示器上着陆的操作相关信息的显示。方法决策显示系统（ADDS）在图形显示中提供动态决策参数，作为所选方法所需设备的健康状况和飞机执行进场和着陆能力的功能。

2. 发明授权

US07751948B2 Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information 有权
标题翻译：显示和接收战术和战略飞行指导信息的装置和方法
公开(公告)号：US07751948B2
公开(公告)日：2010-07-06
申请号：US11639791
申请日：2006-12-14
申请人： Daniel J. Boorman , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
发明人： Daniel J. Boorman , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
IPC分类号： B64C23/00
CPC分类号： G08G5/0021 , G01C23/00 , G08G5/0052
摘要： Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.
摘要翻译：公开了显示和接收战术和战略飞行指导信息的方法和装置。根据本发明的一个方面的方法包括将至少一个第一指示符显示给飞行器的操作者，其中第一指示符对应于由操作者输入的用于指示第一飞行器行为并在接收到激活指令时实现的第一指令从运营商。显示对应于用于将第二飞行器行为至少接近地与第一飞行器行为相同的第二指令的至少一个第二指示符，其中至少一个第二指令将在将来的时间自动实现。至少一个第二指示器至少与至少一个第一指示器大致相同。指标可以分层组织，以简化演示，减少飞行员培训时间。

3. 发明授权

US07256710B2 Methods and systems for graphically displaying sources for and natures of aircraft flight control instructions 有权
标题翻译：用于图形显示飞机飞行控制指令的来源和性质的方法和系统
公开(公告)号：US07256710B2
公开(公告)日：2007-08-14
申请号：US10882800
申请日：2004-06-30
申请人： Randall J. Mumaw , Daniel J. Boorman , William M. Bresley , John C. Griffin, III , Peter D. Gunn
发明人： Randall J. Mumaw , Daniel J. Boorman , William M. Bresley , John C. Griffin, III , Peter D. Gunn
IPC分类号： G01C23/00
CPC分类号： G01C23/00
摘要： Methods and systems for graphically displaying sources for aircraft flight control instructions are disclosed. A method in accordance with one embodiment of the invention includes displaying at a display medium a map of a region at least proximate to an aircraft and displaying an aircraft indicator at least proximate to the map. The aircraft indicator can identify current location of the aircraft, and its location relative to the map can be updated as the aircraft executes a flight. The method can further include displaying at least proximate to the map an indication of a current mode by which a path of the aircraft is currently being automatically controlled.
摘要翻译：公开了用于图形地显示飞行器飞行控制指令的来源的方法和系统。根据本发明的一个实施例的方法包括在显示介质上显示至少靠近飞行器的区域的地图，并且至少在地图附近显示飞行器指示器。飞机指示器可以识别飞机的当前位置，并且当飞机执行飞行时，其相对于地图的位置可以更新。该方法还可以包括至少在地图附近显示飞行器的路径当前正在被自动控制的当前模式的指示。

4. 发明授权

US08364329B2 Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information 有权
标题翻译：显示和接收战术和战略飞行指导信息的装置和方法
公开(公告)号：US08364329B2
公开(公告)日：2013-01-29
申请号：US13419277
申请日：2012-03-13
申请人： Daniel J. Boorman , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
发明人： Daniel J. Boorman , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
IPC分类号： G01C23/00
CPC分类号： G08G5/0021 , G01C23/00 , G08G5/0052
摘要： Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.
摘要翻译：公开了显示和接收战术和战略飞行指导信息的方法和装置。根据本发明的一个方面的方法包括将至少一个第一指示符显示给飞行器的操作者，其中第一指示符对应于由操作者输入的用于指示第一飞行器行为并在接收到激活指令时实现的第一指令从运营商。显示对应于用于将第二飞行器行为至少接近地与第一飞行器行为相同的第二指令的至少一个第二指示符，其中至少一个第二指令将在将来的时间自动实现。至少一个第二指示器至少与至少一个第一指示器大致相同。指标可以分层组织，以简化演示，减少飞行员培训时间。

5. 发明申请

US20110118908A1 METHODS AND SYSTEMS FOR MANAGEMENT OF AIRPLANE SPEED PROFILE 审中-公开
标题翻译：飞机速度剖面管理方法与系统
公开(公告)号：US20110118908A1
公开(公告)日：2011-05-19
申请号：US12621298
申请日：2009-11-18
申请人： Daniel J. BOORMAN , Peter D. GUNN , Randall J. MUMAW
发明人： Daniel J. BOORMAN , Peter D. GUNN , Randall J. MUMAW
IPC分类号： G05D1/00 , G06F17/00
CPC分类号： G08G5/0021 , G08G5/0052 , Y02T50/84
摘要： Methods and systems for airplane speed profile management are disclosed. A method and system in accordance to one embodiment of the disclosure includes a graphical display of speed segments and constraints as well as controls for managing the speeds and associated constraints. Speed Profile Management System (SPMS) provides an integrated and interactive speed profile management tool where pilots can view, update, or change the speed profile of their airplane's current or subsequent phases of flight.
摘要翻译：公开了用于飞机速度轮廓管理的方法和系统。根据本公开的一个实施例的方法和系统包括速度段和约束的图形显示以及用于管理速度和相关约束的控制。速度配置文件管理系统（SPMS）提供了一个集成的交互式速度配置文件管理工具，其中飞行员可以查看，更新或更改飞机当前或后续飞行阶段的速度曲线。

6. 发明授权

US07945354B2 Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information 有权
标题翻译：显示和接收战术和战略飞行指导信息的装置和方法
公开(公告)号：US07945354B2
公开(公告)日：2011-05-17
申请号：US12825135
申请日：2010-06-28
申请人： Daniel J. Boorman , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
发明人： Daniel J. Boorman , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
IPC分类号： G01C23/00
CPC分类号： G08G5/0021 , G01C23/00 , G08G5/0052
摘要： Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.
摘要翻译：公开了显示和接收战术和战略飞行指导信息的方法和装置。根据本发明的一个方面的方法包括将至少一个第一指示符显示给飞行器的操作者，其中第一指示符对应于由操作者输入的用于指示第一飞行器行为并在接收到激活指令时实现的第一指令从运营商。显示对应于用于将第二飞行器行为至少接近地与第一飞行器行为相同的第二指令的至少一个第二指示符，其中至少一个第二指令将在将来的时间自动实现。至少一个第二指示器至少与至少一个第一指示器大致相同。指标可以分层组织，以简化演示，减少飞行员培训时间。

7. 发明申请

US20090062972A1 Systems and Methods for Presenting and Obtaining Flight Control Information 有权
标题翻译：提供和获取飞行控制信息的系统和方法
公开(公告)号：US20090062972A1
公开(公告)日：2009-03-05
申请号：US12260888
申请日：2008-10-29
申请人： Daniel J. Boorman , William M. Bresley , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
发明人： Daniel J. Boorman , William M. Bresley , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
IPC分类号： G05D1/00 , G01C21/00
CPC分类号： G01C23/00 , G01D7/00
摘要： Systems and methods for presenting and obtaining flight control information are disclosed. In one embodiment, information corresponding to a vertical motion of the aircraft can be displayed between information corresponding to a lateral motion of the aircraft and information corresponding to an airspeed of the aircraft. The information displayed can include a current mode for controlling the motion of the aircraft, a current target to which the aircraft is being directed and, at least proximate to both the current mode and the current target, a subsequent target to which the aircraft will be directed after attaining the current target.
摘要翻译：公开了提供和获取飞行控制信息的系统和方法。在一个实施例中，可以在对应于飞行器的横向运动的信息和对应于飞行器的空速的信息之间显示与航空器的垂直运动相对应的信息。显示的信息可以包括用于控制飞行器的运动的当前模式，飞行器正在被引导的当前目标，并且至少接近当前模式和当前目标两者，飞行器将继续到目标在达到目标后执行。

8. 发明授权

US07460029B2 Systems and methods for presenting and obtaining flight control information 有权
标题翻译：提供和获取飞行控制信息的系统和方法
公开(公告)号：US07460029B2
公开(公告)日：2008-12-02
申请号：US10746883
申请日：2003-12-24
申请人： Daniel J. Boorman , William M. Bresley , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
发明人： Daniel J. Boorman , William M. Bresley , John C. Griffin, III , Peter D. Gunn , Randall J. Mumaw
IPC分类号： G01C23/00
CPC分类号： G01C23/00 , G01D7/00
摘要： Systems and methods for presenting and obtaining flight control information are disclosed. In one embodiment, information corresponding to a vertical motion of the aircraft can be displayed between information corresponding to a lateral motion of the aircraft and information corresponding to an airspeed of the aircraft. The information displayed can include a current mode for controlling the motion of the aircraft, a current target to which the aircraft is being directed and, at least proximate to both the current mode and the current target, a subsequent target to which the aircraft will be directed after attaining the current target.
摘要翻译：公开了提供和获取飞行控制信息的系统和方法。在一个实施例中，可以在对应于飞行器的横向运动的信息和对应于飞行器的空速的信息之间显示与航空器的垂直运动相对应的信息。显示的信息可以包括用于控制飞行器的运动的当前模式，飞行器正在被引导的当前目标，并且至少接近当前模式和当前目标两者，飞行器将继续到目标在达到目标后执行。

9. 发明授权

US08423207B2 Integrated approach navigation system, method, and computer program product 有权
标题翻译：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
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： G05D1/00 , G05D1/06 , G05D3/00 , G06F17/00
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。

10. 发明申请

US20110313600A1 INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT 有权
标题翻译：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
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
IPC分类号： G01C23/00 , G05D1/00
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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