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1. 发明授权

EP3959705B1 SYSTEM AND METHOD FOR AUTOMATED TAKE-OFF AND LANDING OF A HIGH ALTITUDE LONG ENDURANCE AIRCRAFT BASED ON THE LOCAL ENVIRONMENT 有权
公开(公告)号：EP3959705B1
公开(公告)日：2024-04-24
申请号：EP20841571.1
申请日：2020-04-23
IPC分类号： G05D1/06 , G08G5/00 , G05D1/02 , G01S13/95
CPC分类号： G05D1/0653 , G08G5/0069 , G08G5/025 , G08G5/0065 , G08G5/0091 , G08G5/0026 , G08G5/0013 , B64U2201/2020230101 , B64U10/25

2. 发明公开

EP3367137A2 SYSTEMS AND METHODS OF GATHERING AND DISTRUBTING CRITICAL WEATHER EVENT INFORMATION 有权
公开(公告)号：EP3367137A2
公开(公告)日：2018-08-29
申请号：EP18157979.8
申请日：2018-02-21
申请人： Honeywell International Inc.
发明人： KODURU, Anantha Chandrasekhar , JONGSMA, Kenneth R. , NARAYANAN, Sibu Parakkattu , DATTA, Subhadip , GUDLA, Siva
IPC分类号： G01W1/00 , G08G5/00 , G01C23/00 , G01W1/08
CPC分类号： G08G5/0013 , G01C21/20 , G01C23/00 , G01S13/953 , G01W1/00 , G01W1/06 , G01W1/08 , G01W2001/006 , G08G5/0008 , G08G5/0021 , G08G5/0026 , G08G5/0034 , G08G5/0047 , G08G5/0052 , G08G5/0091
摘要： A method of gathering and distributing critical weather event information is provided. The method includes monitoring for critical weather events based on defined critical weather event thresholds with an onboard producer weather detection unit of at least one producer vehicle. The critical weather event thresholds are dynamically reconfigured based at least in part on consumption needs of the consumer vehicle. The detected critical weather event and associated time stamp and geolocation information are communicated to a base station. The detected critical weather event is fused with other weather data at the base station to produce a unified weather event image that includes the detected critical weather event. Prediction algorithms are applied to the unified weather event image and are parsed into predefined grid cells of a geo-spatial grid. The predicted weather data is up-linked to a consumer vehicle anticipated to travel within at least one grid cell of the geo-spatial grid.

3. 发明公开

EP3330736A1 DATA COMMUNICATION BETWEEN AIRPORT SURVEILLANCE RADAR AND ONBOARD AIRBORNE WEATHER RADAR 审中-实审
公开(公告)号：EP3330736A1
公开(公告)日：2018-06-06
申请号：EP17202467.1
申请日：2017-11-18
申请人： Honeywell International Inc.
发明人： GHAROTE, Yogesh Prabhakar , RAMACHANDRA, Venkatesh
IPC分类号： G01S13/91 , G01S13/95 , G08G5/00 , G01S7/00
CPC分类号： G08G5/0013 , G01S7/003 , G01S13/913 , G01S13/953 , G08G5/0026 , G08G5/0065 , G08G5/0082 , G08G5/0086 , G08G5/0091 , G08G5/025 , Y02A90/18
摘要： This disclosure is directed to weather radar (40A,B) configured to act as a communication device to allow real time data communication. This disclosure describes using weather radar on board aircraft as a high bandwidth X-band radio for communication. The X-band weather radar is used for receiving flight related data and weather-related data while still acting as a weather radar. As the weather radar system is already present on most commercial aircraft, there is no requirement for additional hardware, devices or equipment onboard the aircraft to meet the data communication needs. An airport may install an X-band data transmitter to broadcast digital data received from detection systems at or near an airport such as an Automated Weather Observing System (AWOS), predictive wind shear (PWS) and bird strike warning systems.

4. 发明公开

EP3314344A1 SYSTEM FOR AUTONOMOUS OPERATION OF MULTIPLE HYBRID UNMANNED AERIAL VEHICLES SUPPORTED BY RECHARGING STATIONS TO PERFORM SERVICES 有权转让
标题翻译：补充站支持执行多种混合无人机的自主操作系统
公开(公告)号：EP3314344A1
公开(公告)日：2018-05-02
申请号：EP16815322.9
申请日：2016-06-23
申请人： Archon Technologies S.r.l. , Venturelli, Davide
发明人： VENTURELLI, Davide
IPC分类号： G05D1/00
CPC分类号： G05D1/104 , B64C25/34 , B64C39/024 , B64C2201/042 , B64C2201/141 , G06Q10/06311 , G06Q10/08 , G08G5/0004 , G08G5/0013 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/0069 , G08G5/0082 , G08G5/0091
摘要： An automated system and method for controlling a plurality of unmanned aerial vehicles (UAVs) is described. The system can include a receiver, a transmitter, and at least one processor in communication with a memory. The receiver receives first telemetric data from the plurality of UAVs. The transmitter is configured to transmit control data to the plurality of UAVs. The memory stores processor-issuable instructions to: substantially simultaneously determine a plurality of plans for each of the plurality of UAVs and for a predetermined time period based at least on the first telemetric data; and iteratively revise the plurality of plans.

5. 发明公开

EP3296978A1 SYSTEM AND METHOD FOR INTELLIGENTLY MINING INFORMATION AND BRIEFING AN AIRCREW ON CONDITIONS OUTSIDE THE AIRCRAFT 无效
标题翻译：系统和方法，用于在飞机外部条件下智能地挖掘信息并简要介绍AIRCREW
公开(公告)号：EP3296978A1
公开(公告)日：2018-03-21
申请号：EP17191216.5
申请日：2017-09-14
申请人： Honeywell International Inc.
发明人： WHITLOW, Stephen , PEPITONE, Dave
IPC分类号： G08G5/00
CPC分类号： G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0078 , G08G5/0086 , G08G5/0091
摘要： A system and method intelligently mines information and briefs an aircrew on conditions outside the aircraft. A mission information manager proactively mines incoming data sources, filters for relevance to current flight, retrieves the most up-to-date information, dynamically selects an appropriate format based on perceptual/cognitive affordances of content, and presents integrated, intuitive data that allows the flight crew to rapidly acquire relevant awareness of conditions outside the aircraft. An expert mission model system reviews incoming information for any situations that are of immediate mission concern. The system presents this information to the flight crew's attention while they have the greatest operational flexibility. Additionally, a human factors module provides decision aiding for select critical phases while taking into account information both outside and inside the aircraft.
摘要翻译：一种系统和方法智能地挖掘信息并在飞机外部的条件下向机组人员简要介绍。任务信息管理器主动挖掘传入的数据源，与当前航班相关的过滤器，检索最新信息，根据内容的感知/认知可供性动态选择适当的格式，并提供集成的直观数据，飞行机组人员能够迅速获得飞机外部条件的相关意识。一个专家任务模型系统审查任何关心的紧急情况的传入信息。该系统将这些信息提供给机组人员的注意力，同时具有最大的操作灵活性。此外，人为因素模块提供决策帮助选择关键阶段，同时考虑飞机外部和内部的信息。

6. 发明公开

EP3267662A1 SYSTEMS AND METHODS FOR COMMUNICATING DATA FROM OFF-VEHICLE DATA SOURCES TO A VEHICLE 无效
标题翻译：用于将车外数据源中的数据传送到车辆的系统和方法
公开(公告)号：EP3267662A1
公开(公告)日：2018-01-10
申请号：EP17177545.5
申请日：2017-06-22
申请人： Honeywell International Inc.
发明人： GOLDSTEIN, David B. , NICHOLLS, James Alexander , DUSIK, Matej , INNOCENT, Simon , RAJE, Anup , NELSON, Bill
IPC分类号： H04L29/08 , G08G5/00
CPC分类号： H04L67/146 , G08G5/0013 , G08G5/0052 , G08G5/0091 , H04L67/06 , H04L67/10 , H04L67/42
摘要： Systems and methods for communicating data from off-vehicle data sources to a vehicle are provided. In one embodiment, a method for obtaining data for a vehicle comprises: initiating an information request from on-board a vehicle; formatting the information request onboard the vehicle into a data file format to generate a request file; performing a wireless file transfer of the request file from the vehicle to a data center, wherein the request file is transferred to a file system location; polling the file system location for creation of a response file corresponding to the request file; when the response file is detected within the file system location, retrieving the response file from the data center to the vehicle; and displaying at the vehicle information responsive to the information request from the response file. In some embodiments, the file system location is a file system location uniquely associated with the vehicle.
摘要翻译：提供了用于从车外数据源向车辆传送数据的系统和方法。在一个实施例中，一种用于获得车辆数据的方法包括：从车载车辆发起信息请求; 将车辆上的信息请求格式化为数据文件格式以生成请求文件; 执行从车辆到数据中心的请求文件的无线文件传输，其中请求文件被传输到文件系统位置; 轮询文件系统位置以创建对应于请求文件的响应文件; 当在文件系统位置内检测到响应文件时，从数据中心向车辆检索响应文件; 以及响应于来自响应文件的信息请求在车辆上显示信息。在一些实施例中，文件系统位置是与车辆唯一关联的文件系统位置。

7. 发明公开

EP3267424A1 METHOD FOR OPERATING AN AT LEAST TEMPORARILY UNMANNED AIRCRAFT OR SPACECRAFT AND AN AIRCRAFT OR SPACECRAFT OF THIS TYPE 审中-公开
标题翻译：用于操作至少暂时无人飞机或航天器以及这种类型的飞机或航天器的方法
公开(公告)号：EP3267424A1
公开(公告)日：2018-01-10
申请号：EP17179323.5
申请日：2017-07-03
申请人： Airbus Defence and Space GmbH
发明人： MEYER, Jörg , HEUER, Thomas , LOHMILLER, Winfried
IPC分类号： G08G5/00
CPC分类号： G08G5/0056 , B64C39/024 , B64F5/60 , G05D1/0011 , G05D1/0055 , G08G5/0013 , G08G5/0039 , G08G5/0052 , G08G5/0069 , G08G5/0091 , H04B7/18506
摘要： The invention relates to a method for operating an at least temporarily unmanned aircraft or spacecraft (10), wherein a flight procedure of the aircraft or spacecraft (10) is carried out in controlled airspace using a previously cleared flight plan, wherein a C2 link (12, 14, 16), via which the aircraft or spacecraft (10) can be or is controlled, is at least temporarily unavailable, and wherein at least one sensor device of the aircraft or spacecraft (10) identifies a dangerous and/or emergency situation which makes it necessary to deviate from the cleared flight plan. To have available a method which makes it possible for an at least temporarily unmanned aircraft or spacecraft to react independently to particular dangerous and/or emergency situations and to avoid damaging events, it is proposed that a control device of the aircraft or spacecraft (10) independently uses a wireless data link (30) to a supervisory authority (31) in order to agree a changed flight plan containing at least one change.
摘要翻译：本发明涉及一种用于操作至少暂时无人驾驶的飞机或航天器（10）的方法，其中使用先前清除的飞行计划在受控空域中执行飞行器或航天器（10）的飞行程序，其中C2链路（10）的至少一个传感器装置至少暂时不可用，并且其中飞机或航天器（10）的至少一个传感器装置识别危险和/或紧急情况这使得有必要偏离已清除的飞行计划。为了使可用的方法能够使至少暂时无人驾驶的飞机或航天器独立地对特定危险和/或紧急情况作出反应并避免损坏事件，建议将飞机或航天器（10）的控制装置独立地使用无线数据链路（30）到监督机构（31）以便同意包含至少一个改变的改变的飞行计划。

8. 发明公开

EP3137856A4 METHOD AND SYSTEM FOR DETECTING AIRCRAFT INDUCED WAKE TURBULENCE 审中-实审
公开(公告)号：EP3137856A4
公开(公告)日：2017-12-27
申请号：EP15786557
申请日：2015-04-21
申请人： WINDBIDCO PTY LTD
发明人： MARTIN ANDREW LOUIS
IPC分类号： G01S15/88 , B64F1/36
CPC分类号： G01S15/885 , B64F1/36 , G01N29/02 , G01N2291/0215 , G01N2291/044 , G01S15/003 , G01S15/104 , G01W1/00 , G01W2001/003 , G08G5/0091
摘要： A method is disclosed for detecting atmospheric turbulence including aircraft induced wake turbulence and/or wind shear within an aperture associated with an aircraft approach or departure corridor around an airport. The method comprises transmitting into the aperture acoustic signals having a waveform suitable for pulse compression and receiving backscattered acoustic echoes of the acoustic signals from the atmospheric turbulence and/or wind shear. The method further includes processing the acoustic echoes in a matched filter receiver to provide a measure of the atmospheric turbulence and discriminating the aircraft induced demise time, being a time taken for the aircraft induced wake turbulence and/or wind shear to fall below a set threshold at least in the aperture. A system for detecting atmospheric turbulence including aircraft induced wake turbulence and/or wind shear associated with an aircraft approach or departure corridor around an airport is also disclosed.

9. 发明公开

EP3249631A1 METHOD AND DEVICE FOR CONTROLLING UNMANNED AERIAL VEHICLE 有权
标题翻译：用于控制无人机的方法和装置
公开(公告)号：EP3249631A1
公开(公告)日：2017-11-29
申请号：EP17156702.7
申请日：2017-02-17
申请人： Beijing Xiaomi Mobile Software Co., Ltd.
发明人： WANG, Weizhao , XIE, Yan , CHU, Yueyue
IPC分类号： G08G5/00 , G05D1/00 , B64C13/16
CPC分类号： G08G5/0069 , B64C13/16 , B64C39/024 , B64C2201/125 , B64C2201/141 , G05D1/102 , G05D1/106 , G08G5/0021 , G08G5/0039 , G08G5/0056 , G08G5/0091
摘要： The present disclosure relates to a method and device for controlling an unmanned aerial vehicle. The method includes: obtaining (101) meteorological data in a current location of the UAV when the UAV is in a first flight state, the first flight state being used to represent a steady flight state or a take-off preparing state of the UAV; determining (102) a flight hazard level of the UAV based on the meteorological data obtained, the flight hazard level being used to represent a hazard level caused to a flight of the UAV by different weather; and controlling (103) the UAV to switch to a second flight state when the flight hazard level is a first preset level, the first preset level representing a level where the UAV cannot fly safely and the second flight state representing an emergency flight state or a take-off suspended state of the UAV.
摘要翻译：本公开涉及用于控制无人飞行器的方法和设备。该方法包括：当UAV处于第一飞行状态时，获得（101）UAV的当前位置中的气象数据，第一飞行状态用于表示UAV的稳定飞行状态或起飞准备状态; 基于获得的气象数据确定（102）所述UAV的飞行危险等级，所述飞行危险等级用于表示由不同天气对所述UAV的飞行造成的危险等级; 以及当所述飞行风险等级是第一预设等级时，控制（103）所述UAV切换到第二飞行状态，所述第一预设等级代表所述UAV不能安全飞行的等级，并且所述第二飞行状态代表紧急飞行状态或起飞暂停状态的无人机。

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