公开(公告)号：EP4365792A1

公开(公告)日：2024-05-08

申请号：EP23204777.9

申请日：2023-10-20

申请人： The Boeing Company

发明人： Brown, Jonathan M.

IPC分类号： G06Q10/047 ,  G01C21/00 ,  G06Q50/40 ,  G08G5/00

CPC分类号： G01C21/005 ,  G08G5/003 ,  G06Q10/047 ,  G06Q50/40

摘要： A method for flight constraints service includes receiving data items at a first computer, transforming the data items into formatted items, transforming metadata items associated with constraints into the formatted items, storing the formatted items in a database, receiving a request at the first computer to view a requested formatted item, generating a geospatial data interchange format file from the requested formatted item, transferring the geospatial data interchange format file from the first computer to a second computer, creating a visual presentation of the geospatial data interchange format file with the second computer, and presenting the visual presentation in a human-readable format at an output device. The data items have multiple data types. The formatted items includes multiple constraints. The constraints include multiple first constraints and multiple second constraints. The metadata items include at least two among effectivity, versioning, timestamps, source, and operational state of the constraints.

公开(公告)号：EP3483858A2

公开(公告)日：2019-05-15

申请号：EP18192968.8

申请日：2018-09-06

申请人： Sikorsky Aircraft Corporation

发明人： WARD, Marc D. ,  LAMPAZZI, Margaret M. ,  SAHAY, Prateek ,  BURDIS, John M.

IPC分类号： G08G5/00 ,  G01S13/94

CPC分类号： G08G5/003 ,  G01S17/933 ,  G06F3/04883 ,  G08G5/0021 ,  G08G5/0034 ,  G08G5/0039 ,  G08G5/045

摘要： A non-transitory computer readable medium includes computer executable instructions for performing a method, the method comprising generating a graphical user interface (GUI) on a display. The GUI can be configured to display aircraft route information and to receive one or more real-time aircraft route inputs. The method also includes receiving, at the GUI, the one or more real-time aircraft route inputs from an input device and conforming the one or more real-time aircraft route inputs to a conformed route. The method includes outputting a conformed route to at least one of the GUI and/or an aircraft control system.

公开(公告)号：EP3407332A1

公开(公告)日：2018-11-28

申请号：EP18173394.0

申请日：2018-05-21

申请人： GE Aviation Systems LLC

发明人： BORGYOS, Szabolcs Andras ,  HOCHWARTH, Joachim Karl Ulf

IPC分类号： G08G5/00 ,  G01C23/00

CPC分类号： G08G5/003 ,  B64D43/00 ,  G01C21/20 ,  G01C23/00 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0052 ,  G08G5/0091

摘要： A method 700 for determining uncertainty in a predicted flight path 400 for an aerial vehicle 100 can include determining 702, by one or more computing devices 602, uncertainty in a performance model of the aerial vehicle 100. The method 700 can further include determining 704, by one or more computing devices 602, uncertainty in a weather model indicative of weather conditions along the predicted flight path 400. In addition, the method 700 can include determining 706, by the one or more computing devices 602, uncertainty in the predicted flight path 400 based on the uncertainty in the performance model and the uncertainty in the weather model. The method 700 can further include generating 708, by one or more computing devices, a notification indicating the uncertainty in the predicted flight path 400.

公开(公告)号：EP2902991B1

公开(公告)日：2017-11-29

申请号：EP15152017.8

申请日：2015-01-21

申请人： Honeywell International Inc.

发明人： McCullough, Sue ,  Sivaratri, Mahesh

IPC分类号： G10L15/26 ,  G08G5/00 ,  G10L15/22

CPC分类号： B64D43/00 ,  B64D31/04 ,  G06F3/167 ,  G08G5/0021 ,  G08G5/003 ,  G10L15/00 ,  G10L15/08 ,  G10L15/22 ,  G10L15/26 ,  G10L2015/085 ,  G10L2015/223 ,  G10L2015/228

摘要： A system and method are provided for programming a flight management system in response to a voice input. The voice input is validated (the pilot spoken vocabulary is thereby filtered (e.g., adapted) to improve recognition accuracy and reduce false positives) by comparing the current operational state of the aircraft (for example, climb, level flight, descent, speed, altitude, and heading), operation validities and availabilities (for example, operations allowed and not allowed) based on the flight management system planned and predicted lateral and vertical trajectory of the flight route (flight plan) from origin/present position to destination, and the requested action being taken.

公开(公告)号：EP2780668B1

公开(公告)日：2017-11-01

申请号：EP12867465.2

申请日：2012-11-15

申请人： Lockheed Martin Corporation ,  Pangilinan, Lester, J. ,  Olsen, John

发明人： PANGILINAN, Lester, J. ,  OLSEN, John

IPC分类号： G01C23/00 ,  G08G5/00

CPC分类号： B64C19/00 ,  G01C23/00 ,  G05D1/0088 ,  G06F3/0227 ,  G06F17/00 ,  G06F21/84 ,  G08G5/0021 ,  G08G5/003 ,  H04B1/3877

摘要： A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component. Each FMS component can have a processor programmed to execute an FMS software product. The FMS can also include a multi core FMS manager configured to control a plurality of flight management systems and coupled to the plurality of FMS components. The multi core FMS manager can include a plurality of FMS managers, each coupled to one of the FMS components, and a platform interface manager coupled to an avionics system. Each FMS manager can be adapted to transmit flight management data.

公开(公告)号：EP3232157A1

公开(公告)日：2017-10-18

申请号：EP17166184.6

申请日：2017-04-12

申请人： GE Aviation Systems LLC

发明人： CABELLO, Juan Jose

IPC分类号： G01C21/20 ,  B25J9/02 ,  B25J9/16

CPC分类号： G08G5/0047 ,  G01C21/20 ,  G01S19/43 ,  G01S19/47 ,  G01S19/51 ,  G08G5/003

摘要： Systems and methods 200 for determining navigation information for an aircraft are provided. In one embodiment, a method 200 can include accessing 202 a satellite-based positioning signal received at a receiver on an aircraft. The satellite-based positioning signal can be indicative of a distance between a satellite and the receiver. The method can include identifying 204 from the satellite-based positioning signal a first vector associated with a distance between the satellite and the receiver and identifying 206 a second vector from the satellite-based positioning signal associated with a distance between a reference point and the satellite. The method can include generating 208 a kinematic model for determining a geometric position of the aircraft based at least in part on a robotic arm using the first vector and the second vector and determining 210 navigation information for the aircraft based at least in part on the kinematic model.

摘要翻译： 提供了用于确定飞行器的导航信息的系统和方法200。 在一个实施例中，方法200可以包括访问202在飞机上的接收器处接收的基于卫星的定位信号。 基于卫星的定位信号可以指示卫星和接收器之间的距离。 该方法可以包括从基于卫星的定位信号中识别204与卫星和接收器之间的距离相关联的第一矢量，并且从基于卫星的定位信号识别206第二矢量与参考点和卫星之间的距离 。 该方法可以包括：至少部分地基于使用第一矢量和第二矢量的机器人臂来生成（208）用于确定飞行器的几何位置的运动学模型;以及至少部分地基于运动学来确定用于飞机的210导航信息 模型。

公开(公告)号：EP3207535A1

公开(公告)日：2017-08-23

申请号：EP15784001.8

申请日：2015-10-16

申请人： Tyco Fire & Security GmbH

发明人： MUCCI, Anthony

IPC分类号： G08B13/196 ,  G05D1/00 ,  G05D1/02 ,  G06K9/00

CPC分类号： G05D1/0088 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/146 ,  G05D1/0011 ,  G05D1/101 ,  G08B13/19604 ,  G08B13/1965 ,  G08G5/003

摘要： An unmanned aerial vehicle is described and includes a computer carried by the unmanned aerial vehicle to control flight of the unmanned aerial vehicle and at least one sensor. The unmanned aerial vehicle is caused to fly a specific pattern within a facility, receive sensor data from a sensor carried by the vehicle, apply processing to the sensor data to detect an unacceptable level of detected feature differences in features contained in the sensor data with respect to video data previously captured at the same location, determine a new flight instruction for the vehicle based on the processing; and send the new flight instruction for the vehicle to a system for controlling flight of the vehicle.

摘要翻译： 描述了一种无人驾驶飞行器，其包括由无人驾驶飞行器携带的用于控制无人驾驶飞行器和至少一个传感器的飞行的计算机。 使无人驾驶飞行器在设施内飞行特定模式，接收来自车辆携带的传感器的传感器数据，对传感器数据应用处理以检测传感器数据中包含的特征中检测到的特征差异的不可接受水平，确定 基于处理的用于车辆的新飞行指令; 并且将用于车辆的新的飞行指令发送到用于控制车辆的飞行的系统。

公开(公告)号：EP3170055A2

公开(公告)日：2017-05-24

申请号：EP15822865.0

申请日：2015-07-08

申请人： Jarrell, John A.

发明人： Jarrell, John A.

IPC分类号： G05D1/00

CPC分类号： G08G5/0013 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/066 ,  B64C2201/141 ,  B64C2201/146 ,  B64D47/06 ,  B64F1/362 ,  G06Q30/04 ,  G06Q50/30 ,  G08G5/003 ,  G08G5/0069 ,  G08G5/0091

摘要： A computer-implemented method of communicating with an unmanned aerial vehicle includes transmitting a first message via a communications transmitter of a lighting assembly for receipt by an unmanned aerial vehicle. The first message includes an identifier associated with the lighting assembly, and the lighting assembly is located within a proximity of a roadway. The method also includes receiving a second message from the unmanned aerial vehicle via a communications receiver of the lighting assembly. The second message includes an identifier associated with the unmanned aerial vehicle. The method further includes transmitting a third message via the communications transmitter of the lighting assembly for receipt by the unmanned aerial vehicle. The third message includes an indication of an altitude at which the unmanned aerial vehicle should fly.

摘要翻译： 一种与无人驾驶飞行器通信的计算机实现的方法包括经由照明组件的通信发射器发送第一消息以供无人飞行器接收。 第一消息包括与照明组件相关联的标识符，并且照明组件位于道路附近。 该方法还包括经由照明组件的通信接收器从无人驾驶飞行器接收第二消息。 第二消息包括与无人驾驶飞行器相关联的标识符。 该方法进一步包括经由照明组件的通信发射器发送第三消息以由无人驾驶飞行器接收。 第三条消息包括无人驾驶飞行器应该飞行的高度的指示。

公开(公告)号：EP3119123A1

公开(公告)日：2017-01-18

申请号：EP16185825.3

申请日：2015-04-20

申请人： PC-Tel, Inc.

发明人： JOHNSON, Brandon ,  ZIK, James ,  SATOH, Atsushi ,  BLAKE, Buchanan ,  SINGER, Martin H.

IPC分类号： H04W24/08 ,  G01S19/14 ,  G05D1/00

CPC分类号： G05D1/0022 ,  B64C39/02 ,  G01C21/20 ,  G01S19/14 ,  G05D1/0011 ,  G05D1/102 ,  G08G5/003 ,  H04W24/08

摘要： A system, apparatus, and method for the measurement, collection, and analysis of radio signals are provided. A transport host device (610), including an unmanned aerial vehicle, can transport a scanning device (620) into desired locations for autonomously collecting radio data for a wireless network, thereby enabling the rapid interrogation and optimization of the wireless network, including in locations and spatial areas where previously known systems and methods have been impractical or impossible. An antenna system (630), connected to the transport host device (610) or to the scanning device (620), is provided for simulating ground coverage from predetermined elevation parameters in the event, for example, that the transport host device (610) is unable to reach or get within a desired predetermined distance of a point of interest (650).

摘要翻译： 本发明提供一种系统，装置，以及用于测量，收集和无线电信号的分析方法。 的传输主机设备（610），包括无人驾驶飞行器，可输送的扫描设备（620）到所需的位置用于自主收集无线电数据在无线网络中，从而使无线网络的快速询问和优化，包括在位置 和空间区域，以前已知的系统和方法已经不实际或不可能。 连接到输送主机设备（610）的天线系统（630）或所述扫描装置（620）被设置用于在所述事件从预定高度参数模拟地面覆盖，例如，DASS模输送主机设备（610） 无法到达或利息（650）上的点的期望的预定距离之内搞定。

公开(公告)号：EP3051520A1

公开(公告)日：2016-08-03

申请号：EP16152637.1

申请日：2016-01-25

申请人： Honeywell International Inc.

发明人： SAMUTHIRAPANDIAN, Subash ,  JOHNSON, Markus Alan ,  MALVIYA, Pramod Kumar ,  B, Jayasenthilnathan ,  PASSINGER, Bretislav

IPC分类号： G08G5/00 ,  G01C23/00

CPC分类号： G08G5/0021 ,  G01C23/00 ,  G08G5/0013 ,  G08G5/003 ,  G08G5/0039 ,  G08G5/06

摘要： A flight display system or method in accordance with this disclosure involves the presentation, on an aircraft, of a "quick preview" notice to airmen ("NOTAM") display that includes a plurality of stacked flight route portion boxes, each of the plurality of flight route portion boxes pertaining to and being labeled as one of: a departure taxiing portion, a standard instrument departure portion, an en route portion, a standard terminal arrival route portion, an approach portion, and an arrival taxiing portion; each of the plurality of flight route portion boxes graphically displaying flight route symbology pertaining to and labeled as each airport taxiing reference point and/or each aeronautical waypoint that falls within its labeled flight route portion; and wherein at least one of the plurality of flight route portion boxes further graphically displays NOTAM symbology pertaining to at least one of the NOTAMs that are relevant to the flight route.

摘要翻译： 根据本公开的飞行显示系统或方法涉及在飞行器上呈现包括多个堆叠飞行路线部分框的飞行员（“NOTAM”）显示器的“快速预览”通知， 飞行路线部分框，属于以下之一并被标记为：起落滑行部分，标准仪表离开部分，途中部分，标准终点站到达路线部分，接近部分和到达滑行部分; 多个飞行路线部分框中的每一个图形地显示属于并标记为每个机场滑行参考点的飞行路线符号系和/或落在其标记的飞行路线部分内的每个航空航路点; 并且其中所述多个飞行路线部分框中的至少一个进一步图形地显示与与所述飞行路线相关的至少一个所述NOTAM的NOTAM符号系统。