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111. 发明公开

EP3273425A2 METHODS AND APPARATUS FOR FLIGHT BRIEFING DATA SYNCHRONIZATION 失效
标题翻译：用于飞行简报数据同步的方法和装置
公开(公告)号：EP3273425A2
公开(公告)日：2018-01-24
申请号：EP17163449.6
申请日：2017-03-28
申请人： Honeywell International Inc.
发明人： VASEK, Jiri , TIEFTRUNK, Petr , EICHLER, Zdenek , BILEK, Jan
IPC分类号： G08G5/00 , H04L29/06 , H04L29/08
CPC分类号： H04L67/1095 , G08G5/0013 , G08G5/0021 , G08G5/0034 , G08G5/0039 , G08G5/0091 , H04L65/1069 , H04L67/12
摘要： A method for managing a flight briefing data system is provided. The method establishes, by a central computer system, a first communication connection with an electronic device and a second communication connection with an aircraft onboard avionics unit; transmits, by the central computer system, flight briefing data via the first communication connection and the second communication connection, wherein the flight briefing data comprises at least a plurality of Notices to Airmen (NOTAMs) associated with a pending flight; receives, by the central computer system, altered flight briefing data; and synchronizes the central computer system, the electronic device, and the aircraft onboard avionics unit, by transmitting the altered flight briefing data via the first communication connection and the second communication connection.
摘要翻译：提供了一种用于管理飞行简报数据系统的方法。该方法通过中央计算机系统建立与电子设备的第一通信连接以及与飞机机载航空电子设备单元的第二通信连接; 由所述中央计算机系统经由所述第一通信连接和所述第二通信连接传输飞行简报数据，其中所述飞行简报数据包括与待决航班相关联的至少多个通告到航空公司（NOTAM）;以及其中，由中央计算机系统接收改变的飞行简报数据; 并且通过经由第一通信连接和第二通信连接发送改变后的飞行简报数据来同步中央计算机系统，电子设备和飞机机载航空电子设备单元。

112. 发明公开

EP3264392A2 AGGREGATION AND DISTRIBUTION OF REAL-TIME DATA 无效
公开(公告)号：EP3264392A2
公开(公告)日：2018-01-03
申请号：EP17176738.7
申请日：2017-06-19
申请人： Honeywell International Inc.
发明人： SRIVASTAV, Amit , IDUPUNUR, Krishna , NARAYANAN, Sibu Parakkattu , KODURU, Anantha Chandrasekhar , MERCHANT, Shafi
IPC分类号： G08G5/00 , G01W1/02 , G01S13/95
CPC分类号： G08G5/0091 , G01S13/953 , G01W1/02 , G01W2001/006 , G01W2203/00 , G06Q30/0283 , G08G5/0013 , G08G5/0021 , G08G5/0026 , Y02A90/14 , Y02A90/18
摘要： A system for data aggregation and distribution comprises a context builder that receives a data request from a consumer, and a producers locator that communicates with producers. A producers filter receives a list of producers and selects producers capable of providing data relevant to context information. A data requests formatter receives the context information, and sends the data request to the selected producers. A data responses validator validates data responses from producers, and a data responses processor processes validated data responses. A data predictor receives processed data responses and context information, and generates data prediction information. A data fusion module receives processed data responses, context information, data prediction information, and data history. The data fusion module combines processed data responses with data prediction information to generate a consolidated data response for the consumer. The data fusion module also considers data prediction information upon receiving a request for predicted data when real-time data is unavailable.

113. 发明授权

EP2696171B1 Aircraft systems and methods for displaying weather information along a flight path 失效转让
标题翻译：飞行器系统和沿着飞行路径显示天气信息的方法
公开(公告)号：EP2696171B1
公开(公告)日：2017-12-27
申请号：EP13177898.7
申请日：2013-07-24
申请人： Honeywell International Inc.
发明人： Ramaiah, Vinoda , Krishna, Kiran Gopala
IPC分类号： G01C23/00 , G08G5/00 , G01W1/02
CPC分类号： G01W1/02 , G01C23/00 , G08G5/0013 , G08G5/0021 , G08G5/0047 , G08G5/0052 , G08G5/0091
摘要： A display system for an aircraft is provided. The system includes a processing unit configured to receive weather information associated with a flight path of a flight plan and to generate display commands based on the weather information. The flight plan includes a first waypoint associated with a first altitude. The system further includes a display device coupled with the processing unit and configured to receive the display commands and to display symbology representing the weather information. The weather information includes first weather information for the first altitude and second weather information at a second altitude, different from the first altitude.

114. 发明公开

EP3164772A4 SYSTEMS AND METHODS FOR GEO-FENCING DEVICE IDENTIFICATION AND AUTHENTICATION 无效
公开(公告)号：EP3164772A4
公开(公告)日：2017-12-13
申请号：EP15871320
申请日：2015-03-31
申请人： SZ DJI TECHNOLOGY CO LTD
发明人： GONG MING , DAI JIN , CUI HAO , WANG XIAODONG , HUANG HAN , WU JUN , FAN WEI , MA NING , RONG XINHUA , LIN XINGSEN
IPC分类号： G05D1/10 , G06F21/62 , G08G5/00 , G08G5/04 , H04W4/02 , H04W12/06
CPC分类号： G08G5/0091 , B64C39/024 , B64C2201/027 , B64C2201/145 , B64C2201/146 , G05D1/101 , G06F21/6218 , G06F2221/2111 , G06F2221/2117 , G08G5/0008 , G08G5/0013 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/0043 , G08G5/0052 , G08G5/0056 , G08G5/006 , G08G5/0069 , G08G5/0078 , G08G5/0082 , G08G5/0086 , H04W4/022 , H04W12/06
摘要： Systems and methods for UAV safety are provided. An authentication system may be used to confirm UAV and/or user identity and provide secured communications between users and UAVs. The UAVs may operate in accordance with a set of flight regulations. The set of flight regulations may be associated with a geo-fencing device in the vicinity of the UAV.

115. 发明公开

EP3158553A4 AUTHENTICATION SYSTEMS AND METHODS FOR IDENTIFICATION OF AUTHORIZED PARTICIPANTS 有权
公开(公告)号：EP3158553A4
公开(公告)日：2017-11-15
申请号：EP15874415
申请日：2015-03-31
申请人： SZ DJI TECHNOLOGY CO LTD
发明人： GONG MING , DAI JIN , CUI HAO , WANG XIAODONG , HUANG HAN , WU JUN , FAN WEI , MA NING , RONG XINHUA , LIN XINGSEN
IPC分类号： G08G5/00 , B64C39/02 , G05D1/00 , G06F21/31 , G06F21/57 , G06F21/62 , G06F21/73 , G06Q30/00 , G08G5/04 , H04L9/08 , H04L29/06 , H04W4/02 , H04W12/04 , H04W12/06
CPC分类号： G08G5/045 , B64C39/024 , B64C2201/027 , B64C2201/145 , B64C2201/146 , G05D1/0027 , G06F21/31 , G06F21/57 , G06F21/6218 , G06F21/73 , G06F2221/2111 , G06F2221/2117 , G08G5/0008 , G08G5/0013 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/0043 , G08G5/0052 , G08G5/0056 , G08G5/006 , G08G5/0069 , G08G5/0078 , G08G5/0082 , G08G5/0086 , G08G5/0091 , H04L63/0823 , H04L63/083 , H04L63/0892 , H04W4/022 , H04W12/04 , H04W12/06
摘要： Systems and methods for UAV safety are provided. An authentication system may be used to confirm UAV and/or user identity and provide secured communications between users and UAVs. The UAVs may operate in accordance with a set of flight regulations. The set of flight regulations may be associated with a geo-fencing device in the vicinity of the UAV.

116. 发明公开

EP3241205A2 SYSTEM AND METHOD FOR CONTROLLING AUTONOMOUS FLYING VEHICLE FLIGHT PATHS 审中-公开
标题翻译：用于控制自主飞行飞行器飞行路径的系统和方法
公开(公告)号：EP3241205A2
公开(公告)日：2017-11-08
申请号：EP15876241.9
申请日：2015-12-30
申请人： Airmap Inc.
发明人： MARCUS, Benjamin Daniel
IPC分类号： G08G5/00 , B64C39/02
CPC分类号： G08G5/0034 , B64C39/024 , B64C2201/123 , B64C2201/141 , G08G5/0008 , G08G5/0013 , G08G5/0039 , G08G5/006 , G08G5/0069 , G08G5/0078 , G08G5/0091
摘要： A method is provided for limiting access to airspace by drones. The method includes receiving position information from a user associated with a property identified by the position information. The method also includes assembling the position information with other position information to compile a comprehensive configurable flight zone database. The method further includes pushing the configurable flight zone database to at least one drone. The drone accesses the configurable flight zone database to determine if movement is allowed, and the drone is programmed to not fly into areas identified in the configurable flight zone database. In the method, the drone may be further programmed to prohibit directing a camera into the areas identified in the configurable flight zone database.

117. 发明公开

EP3220170A1 REQUESTING WEATHER DATA BASED ON PRE-SELECTED EVENTS 有权
标题翻译：根据预选的事件请求天气数据
公开(公告)号：EP3220170A1
公开(公告)日：2017-09-20
申请号：EP17155933.9
申请日：2017-02-13
申请人： Honeywell International Inc.
发明人： WANG, Guoquing , WANG, Haiming , WANG, Heifeng , LIANG, Danhua
IPC分类号： G01W1/00
CPC分类号： H04B7/18506 , G01C21/20 , G01S7/003 , G01S13/951 , G01S13/953 , G01W1/00 , G01W1/02 , G08G5/0013 , G08G5/0026 , G08G5/0091 , Y02A90/18
摘要： A ground weather center may transmit information requests that carry at least one meteorological specific triggering command. An airborne system may translate the triggering command into detectable meteorological conditions and may arm the trigger(s) for specific weather sensors accordingly and downlink information upon the airborne system detects the triggering conditions. By using such a triggering command, the airborne system may be able transmit the same amount of valuable information with less bandwidth by reducing the number of redundant downlinked packets.
摘要翻译：地面气象中心可以发送携带至少一个气象特定触发命令的信息请求。机载系统可以将触发命令转换为可检测的气象条件，并且可以相应地针对特定的气象传感器设置触发器，并且可以根据机载系统检测触发条件的下行链路信息。通过使用这样的触发命令，机载系统可以通过减少冗余的下行链路分组的数量，以较少的带宽发送相同数量的有价值的信息。

118. 发明公开

EP3046092A4 LANDING DECISION ASSISTANCE SYSTEM, LANDING DECISION ASSISTANCE METHOD, AND LANDING DECISION ASSISTANCE PROGRAM 审中-公开
标题翻译：土地退化，森林退化，土地退化，土地退化，土地退化，土地退化，土地退化
公开(公告)号：EP3046092A4
公开(公告)日：2017-09-13
申请号：EP14844216
申请日：2014-08-11
申请人： JAPAN AEROSPACE EXPLORATION
发明人： IIJIMA TOMOKO , MATAYOSHI NAOKI , YOSHIKAWA EIICHI
IPC分类号： G08G5/02 , B64D45/04 , B64F1/36 , G01S13/89 , G01S13/91 , G01S13/95 , G08G5/00
CPC分类号： B64D45/04 , G01S13/89 , G01S13/913 , G01S13/951 , G01S13/953 , G08G5/0013 , G08G5/0026 , G08G5/0091 , G08G5/025 , Y02A90/18
摘要： There are provided a landing decision support system, a landing decision support method, and a landing decision support program that allow a general user other than a specialist to easily and accurately read information useful for a decision of an aircraft landing. A landing decision support system 1 for providing information for supporting the decision of the aircraft landing has a screen generation unit 220 that generates various screens displayed in a display unit, and a display control unit 260 that causes the display unit to display the various screens generated by the screen generation unit 220, the screen generation unit 220 includes an echo intensity screen generation unit 240 that generates an echo intensity screen, and echo intensity information included in the echo intensity screen is generated based on echo intensity data of an observation target acquired by a weather sensor, and displays a horizontal distribution of an echo intensity using a summary statistic of the echo intensity in an area around an airport in a predetermined altitude range.
摘要翻译：提供了一种着陆决策支持系统，一种着陆决策支持方法和一种着陆决策支持程序，其允许除专家以外的一般用户容易且准确地读取对于飞机着陆的决定有用的信息。用于提供用于支持飞机着陆决定的信息的着陆决定支持系统1具有生成在显示单元中显示的各种画面的画面生成单元220和使显示单元显示生成的各种画面的显示控制单元260 画面生成部220具备生成回波强度画面的回波强度画面生成部240，根据由该画面生成部220生成的观测对象的回波强度数据生成回波强度画面中包含的回波强度信息天气传感器，并且使用在预定高度范围内的机场周围区域中的回波强度的概要统计来显示回波强度的水平分布。

119. 发明授权

EP2955481B1 MÉTHODE ET SYSTÈME EMBARQUÉ DE VISUALISATION DE RISQUES MÉTÉOROLOGIQUES 有权转让
标题翻译： MÉTHODEETSYSTÈMEEMBARQUÉDE VISUALIZATION DE RISQUESMÉTÉOROLOGIQUES
公开(公告)号：EP2955481B1
公开(公告)日：2017-09-13
申请号：EP15171559.6
申请日：2015-06-11
申请人： GTD Sistemas de Informacion
发明人： Bas Gago, Isidro , Dominguez Armesto, Oscar
IPC分类号： G01C21/00 , G01C23/00 , G01S13/95 , G08G5/00 , G01S7/24 , G01W1/10
CPC分类号： B60K35/00 , G01C21/00 , G01C23/00 , G01S7/24 , G01S13/95 , G01W1/10 , G01W2203/00 , G08G5/0047 , G08G5/0091 , Y02A90/18

120. 发明公开

EP3211620A1 METHOD AND ELECTRONIC DEVICE FOR ESTABLISHING OPTIMIZED HOLDING PATTERNS FOR AIRCRAFT 审中-公开
标题翻译：用于建立飞机优化保持模式的方法和电子设备
公开(公告)号：EP3211620A1
公开(公告)日：2017-08-30
申请号：EP16382080.6
申请日：2016-02-26
申请人： The Boeing Company
发明人： DE PRINS, Johan , KLEIN KOERKAMP, Niek , FIGLAR, Bastian
IPC分类号： G08G5/00 , G06Q10/04
CPC分类号： G08G5/0052 , G06Q10/047 , G08G5/0021 , G08G5/0039 , G08G5/0091
摘要： Method and electronic device for establishing optimized holding patterns for aircraft. The electronic device (200, 300) comprises a communication module (210, 310) and an optimization module (220, 320). The communication module (210, 310) receives optimization conditions (108) including aircraft data (110) and atmospheric conditions (120) proximate a holding pattern location.
The optimization module (220, 320), which comprises a cost function generator (222, 322) and cost function optimizer (226, 326), receives a cost function condition (140) and holding pattern optimization parameters (150). The cost function generator (222, 322) generates a cost function (224) with holding pattern optimization parameters (150). The cost function optimizer (226, 326) applies an optimization routine (102) to the cost function (224) considering the optimization conditions (108) to obtain a value for the holding pattern optimization parameters (150) having a minimized cost, obtaining an optimized holding pattern (106).
摘要翻译：用于建立飞机优化保持模式的方法和电子装置。电子设备（200,300）包括通信模块（210,310）和优化模块（220,320）。通信模块（210,310）接收包括靠近保持图案位置的飞机数据（110）和大气条件（120）的优化条件（108）。包括成本函数发生器（222,322）和成本函数优化器（226,326）的优化模块（220,320）接收成本函数条件（140）和保存模式优化参数（150）。成本函数生成器（222,322）利用保持模式优化参数（150）生成成本函数（224）。成本函数优化器（226,326）考虑优化条件（108）将优化例程（102）应用于成本函数（224）以获得具有最小成本的保持模式优化参数（150）的值，获得优化保持模式（106）。

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