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公开(公告)号：US20140114557A1
公开(公告)日：2014-04-24
申请号：US13655407
申请日：2012-10-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , Keith Hughes , Christine Marie Haissig , Daniel Eugene Lewis
IPC: G08G5/06
CPC classification number: G01C21/00 , G05D1/0083 , G08G5/0013 , G08G5/0021 , G08G5/065
Abstract: A high-integrity auto-guidance and control method for use in conjunction with an aircraft electric taxi drive system comprises obtaining taxi path data generating in a plurality of processors taxi path guidance and control information from the taxi path guidance data, and sending commands derived from the taxi path guidance and control information from one of the plurality of processors based on a predetermined priority scheme to at least one electric taxi controller.
Abstract translation: 与飞机电动出租车司机系统一起使用的高度完整的自动引导和控制方法包括：从出租车路线指导数据获得在多个处理器中的出租车路径指导和控制信息生成的出租车路径数据，以及发送命令 所述出租车路径引导和控制信息从所述多个处理器中的一个基于预定优先级方案发送到至少一个电动出租车控制器。
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公开(公告)号：US09406235B2
公开(公告)日：2016-08-02
申请号：US14250022
申请日：2014-04-10
Applicant: Honeywell International Inc.
Inventor： Kevin J Conner , Christine Marie Haissig , Ruy C. Brandao
CPC classification number: G08G5/0017 , G01C21/00 , G01C21/30 , G08G5/0013 , G08G5/0082 , G08G5/065
Abstract: In some examples described herein, a runway location is determined based on aircraft state information from at least one aircraft. For example, a processor may determine the coordinates of one or more points of a runway based on aircraft state information generated by one or more aircraft using the runway. In some examples, the processor may aggregate coordinates determined from the aircraft state information provided by a plurality of different aircraft in order to determine the location of the runway. The processor can be located onboard an aircraft providing the state information, onboard a different aircraft, or external to any aircraft.
Abstract translation: 在本文描述的一些示例中，基于来自至少一架飞行器的飞机状态信息来确定跑道位置。 例如，处理器可以基于由使用跑道的一个或多个飞行器产生的飞行器状态信息来确定跑道的一个或多个点的坐标。 在一些示例中，处理器可以聚集由多个不同飞行器提供的飞行器状态信息确定的坐标，以便确定跑道的位置。 处理器可以位于提供状态信息的飞机上，在不同的飞机上或在任何飞机外部。
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公开(公告)号：US09074891B2
公开(公告)日：2015-07-07
申请号：US13655407
申请日：2012-10-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , Keith Hughes , Christine Marie Haissig , Daniel Eugene Lewis
CPC classification number: G01C21/00 , G05D1/0083 , G08G5/0013 , G08G5/0021 , G08G5/065
Abstract: A high-integrity auto-guidance and control method for use in conjunction with an aircraft electric taxi drive system comprises obtaining taxi path data generating in a plurality of processors taxi path guidance and control information from the taxi path guidance data, and sending commands derived from the taxi path guidance and control information from one of the plurality of processors based on a predetermined priority scheme to at least one electric taxi controller.
Abstract translation: 与飞机电动出租车司机系统一起使用的高度完整的自动引导和控制方法包括：从出租车路线指导数据获得在多个处理器中的出租车路径指导和控制信息生成的出租车路径数据，以及发送命令 所述出租车路径引导和控制信息从所述多个处理器中的一个基于预定优先级方案发送到至少一个电动出租车控制器。
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4.发明申请SYSTEMS AND METHODS FOR IMPROVING POSITIONAL AWARENESS WITHIN AN AIRPORT MOVING MAP 有权用于改善机场移动地图中的位置意识的系统和方法公开(公告)号：US20160236795A1
公开(公告)日：2016-08-18
申请号：US14623004
申请日：2015-02-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Tomas Marczi , Jan Flasar , Juliana Sevcikova , Christine Marie Haissig , Stephen Whitlow , Kevin J Conner , John Howard Glover
IPC: B64D45/00
CPC classification number: B64D45/00 , G01S7/22 , G01S13/931 , G01S2013/916 , G06F3/14 , G06F3/147 , G08G5/0021 , G08G5/045 , G08G5/065 , G09G2340/045 , G09G2340/12 , G09G2380/12
Abstract: Systems and methods for displaying a location reference indicator (LRI) associated with an ownship icon are provided. In various embodiments, an airport moving map (AMM) is displayed, and the ownship icon is displayed in the AMM, where the ownship icon represents the ownship. A degree of zoom of the AMM is determined. In response to a determination that the degree of zoom is not within a range of center referenced threshold values, a first LRI is displayed that indicates that the icon representing the ownship is not to scale with other objects displayed in the AMM. In response to a determination that the degree of zoom is within the range of center referenced threshold values, a second LRI is displayed.
Abstract translation: 提供了用于显示与自身图标相关联的位置参考指示符（LRI）的系统和方法。 在各种实施例中，显示机场移动地图（AMM），并且自身图标显示在AMM中，其中自身图标表示自身。 确定AMM的变焦程度。 响应于缩放程度不在中心参考阈值范围内的确定，显示表示本身的图标不与在AMM中显示的其他对象相比例的第一LRI。 响应于确定变焦度在中心参考阈值的范围内，显示第二LRI。
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公开(公告)号：US20150170525A1
公开(公告)日：2015-06-18
申请号：US14109093
申请日：2013-12-17
Applicant: Honeywell International Inc.
Inventor： Kevin J Conner , Tomas Marczi , Christine Marie Haissig , John Howard Glover
CPC classification number: G08G5/0021 , G08G5/0073 , G08G5/06 , G08G5/065
Abstract: In some examples, a processor is configured to control a ground obstacle collision alerting system of an aircraft to deactivate delivery of ground obstacle collision alerts in response to determining the aircraft is in a designated ground area. In some examples, the processor is configured to determine the aircraft is in the designated ground area based on user input, based on a geographic location of the aircraft, or both. The processor is further configured to control the ground obstacle collision alerting system to automatically reactivate the delivery of the ground obstacle collision alerts in response to determining the aircraft is outside of the designated ground area. In some examples, the processor is configured to determine the aircraft is outside of the designated ground area based on a geographic location of the aircraft, a ground speed of the aircraft, or both.
Abstract translation: 在一些示例中，处理器被配置为响应于确定飞行器在指定的地面区域来控制飞行器的地面障碍物碰撞警报系统以停用地面障碍物碰撞警报的传递。 在一些示例中，处理器被配置为基于飞行器的地理位置或两者来基于用户输入来确定飞行器在指定地面区域。 所述处理器还被配置为响应于确定所述飞机在所述指定的地面以外的区域来控制所述地面障碍物碰撞警报系统以自动地重新启动所述地面障碍物碰撞警报的传递。 在一些示例中，处理器被配置为基于飞机的地理位置，飞机的地面速度或两者来确定飞行器在指定的地面区域之外。
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Patent Agency Ranking
6.发明授权Systems and methods for improving positional awareness within an airport moving map 有权提高机场移动地图位置意识的系统和方法公开(公告)号：US09561865B2
公开(公告)日：2017-02-07
申请号：US14623004
申请日：2015-02-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Tomas Marczi , Jan Flasar , Juliana Sevcikova , Christine Marie Haissig , Stephen Whitlow , Kevin J Conner , John Howard Glover
CPC classification number: B64D45/00 , G01S7/22 , G01S13/931 , G01S2013/916 , G06F3/14 , G06F3/147 , G08G5/0021 , G08G5/045 , G08G5/065 , G09G2340/045 , G09G2340/12 , G09G2380/12
Abstract: Systems and methods for displaying a location reference indicator (LRI) associated with an ownship icon are provided. In various embodiments, an airport moving map (AMM) is displayed, and the ownship icon is displayed in the AMM, where the ownship icon represents the ownship. A degree of zoom of the AMM is determined. In response to a determination that the degree of zoom is not within a range of center referenced threshold values, a first LRI is displayed that indicates that the icon representing the ownship is not to scale with other objects displayed in the AMM. In response to a determination that the degree of zoom is within the range of center referenced threshold values, a second LRI is displayed.
Abstract translation: 提供了用于显示与自身图标相关联的位置参考指示符（LRI）的系统和方法。 在各种实施例中，显示机场移动地图（AMM），并且自身图标显示在AMM中，其中自身图标表示自身。 确定AMM的变焦程度。 响应于缩放程度不在中心参考阈值范围内的确定，显示表示本身的图标不与在AMM中显示的其他对象相比例的第一LRI。 响应于确定变焦度在中心参考阈值的范围内，显示第二LRI。
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公开(公告)号：US20150294573A1
公开(公告)日：2015-10-15
申请号：US14250022
申请日：2014-04-10
Applicant: Honeywell International Inc.
Inventor： Kevin J Conner , Christine Marie Haissig , Ruy C. Brandao
CPC classification number: G08G5/0017 , G01C21/00 , G01C21/30 , G08G5/0013 , G08G5/0082 , G08G5/065
Abstract: In some examples described herein, a runway location is determined based on aircraft state information from at least one aircraft. For example, a processor may determine the coordinates of one or more points of a runway based on aircraft state information generated by one or more aircraft using the runway. In some examples, the processor may aggregate coordinates determined from the aircraft state information provided by a plurality of different aircraft in order to determine the location of the runway. The processor can be located onboard an aircraft providing the state information, onboard a different aircraft, or external to any aircraft.
Abstract translation: 在本文描述的一些示例中，基于来自至少一架飞行器的飞机状态信息来确定跑道位置。 例如，处理器可以基于由使用跑道的一个或多个飞行器产生的飞行器状态信息来确定跑道的一个或多个点的坐标。 在一些示例中，处理器可以聚集由多个不同飞行器提供的飞行器状态信息确定的坐标，以便确定跑道的位置。 处理器可以位于提供状态信息的飞机上，在不同的飞机上或在任何飞机外部。
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公开(公告)号：US08935018B2
公开(公告)日：2015-01-13
申请号：US14083706
申请日：2013-11-19
Applicant: Honeywell International Inc.
Inventor： Keith Hughes , Joseph Nutaro , Christine Marie Haissig
CPC classification number: G05D1/0202 , G05D1/0083
Abstract: An auto-guidance and control method and system are provided for use in conjunction with an aircraft electric taxi system, wherein electric taxi guidance may be performed in a manual mode by a crew or in an auto-mode by an auto-guidance and control system. First, aircraft status data and airport feature data are accessed. A processor, in response to at least the aircraft status data and the airport feature data, generates taxi guidance information and renders the taxi guidance information on a display. A guidance route is manually navigated utilizing guidance information on the display in the manual mode. In the auto mode, taxi-path commands, generated by the processor, are applied to taxi path guidance controllers in the auto-mode.
Abstract translation: 提供了一种与飞机电动出租车系统一起使用的自动引导和控制方法和系统，其中电动出租车引导可以由船员以手动方式执行，或者通过自动引导和控制系统以自动模式执行 。 首先，访问飞机状态数据和机场特征数据。 响应于至少飞机状态数据和机场特征数据的处理器产生出租车指导信息，并将出租车引导信息呈现在显示器上。 使用手动模式下的显示器上的指导信息手动导航指导路线。 在自动模式下，由处理器生成的滑行路径命令以自动模式应用于出租车路径引导控制器。
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9.发明申请METHODS AND APPARATUS FOR DETERMINING AND USING A LANDING SURFACE FRICTION CONDITION 审中-公开用于确定和使用着陆表面摩擦条件的方法和装置公开(公告)号：US20160140854A1
公开(公告)日：2016-05-19
申请号：US14223579
申请日：2014-03-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Dale Frederick Enns , Yasuo Ishihara , Donald Carl Kauffman , Kenneth R. Jongsma , Christine Marie Haissig
CPC classification number: G08G5/025 , G01S13/74 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0086 , G08G5/0091
Abstract: A diagnostic method performed onboard an aircraft is provided. The method obtains aircraft state data during landing of the aircraft, via a plurality of avionics and aircraft systems; and determines a landing surface friction condition based on the aircraft state data, using at least one of the plurality of avionics and aircraft systems. A method of evaluating landing surface data onboard an aircraft is also provided. The method receives landing surface friction condition data, prior to landing; computes a required landing distance, based on the received landing surface friction condition data; and when the required landing distance is more than a predetermined threshold, performs a designated task.
Abstract translation: 提供了一种在飞机上执行的诊断方法。 该方法通过多个航空电子设备和飞行器系统在飞机着陆期间获得飞行器状态数据; 并且使用所述多个航空电子设备和飞行器系统中的至少一个来确定基于飞行器状态数据的着陆面摩擦条件。 还提供了一种评估飞机上的着陆面数据的方法。 该方法在着陆前接收着陆面摩擦条件数据; 基于所接收的着陆面摩擦条件数据计算所需的着陆距离; 并且当所需的着陆距离大于预定阈值时，执行指定的任务。
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公开(公告)号：US09318025B2
公开(公告)日：2016-04-19
申请号：US14109093
申请日：2013-12-17
Applicant: Honeywell International Inc.
Inventor： Kevin J Conner , Tomas Marczi , Christine Marie Haissig , John Howard Glover
CPC classification number: G08G5/0021 , G08G5/0073 , G08G5/06 , G08G5/065
Abstract: In some examples, a processor is configured to control a ground obstacle collision alerting system of an aircraft to deactivate delivery of ground obstacle collision alerts in response to determining the aircraft is in a designated ground area. In some examples, the processor is configured to determine the aircraft is in the designated ground area based on user input, based on a geographic location of the aircraft, or both. The processor is further configured to control the ground obstacle collision alerting system to automatically reactivate the delivery of the ground obstacle collision alerts in response to determining the aircraft is outside of the designated ground area. In some examples, the processor is configured to determine the aircraft is outside of the designated ground area based on a geographic location of the aircraft, a ground speed of the aircraft, or both.
Abstract translation: 在一些示例中，处理器被配置为响应于确定飞行器在指定的地面区域来控制飞行器的地面障碍物碰撞警报系统以停用地面障碍物碰撞警报的传递。 在一些示例中，处理器被配置为基于飞行器的地理位置或两者来基于用户输入来确定飞行器在指定地面区域。 所述处理器还被配置为响应于确定所述飞机在所述指定的地面以外的区域来控制所述地面障碍物碰撞警报系统以自动地重新启动所述地面障碍物碰撞警报的传递。 在一些示例中，处理器被配置为基于飞机的地理位置，飞机的地面速度或两者来确定飞行器在指定的地面区域之外。
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