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1. 发明公开

EP3223103A1 MISSION PARAMETERIZATION SYSTEM 审中-公开
标题翻译：任务参数化系统
公开(公告)号：EP3223103A1
公开(公告)日：2017-09-27
申请号：EP17160822.7
申请日：2017-03-14
申请人： Sikorsky Aircraft Corporation
发明人： PITCHER, Garrett , WARD, Mark D.
IPC分类号： G05D1/06 , G01S13/91 , G06K9/00 , G06T7/73 , G08G5/02 , G08G5/00 , G01C23/00 , G01S17/93
CPC分类号： G08G5/003 , G01C23/00 , G01S13/913 , G01S17/933 , G05D1/0088 , G05D1/101 , G06K9/00637 , G06T7/73 , G08G5/0021 , G08G5/0073 , G08G5/025
摘要： A system for mission parameterization is provided and includes a vehicle that itself includes a sensor to sense characteristic sensed elements in surroundings of the vehicle and a computing device. The computing device includes a processing unit and a memory unit. The memory unit has a database configured to associate objects disposable in the surroundings with sensible characteristic object elements and executable instructions. The executable instructions are configured to cause the processing unit to find correspondence between any characteristic sensed elements in the surroundings, which are sensed by the activated sensor, and any of the characteristic object elements, identify objects in the surroundings based on the correspondence and set mission parameters based on identifications of the objects in the surroundings.
摘要翻译：提供了用于任务参数化的系统，并且该系统包括车辆，该车辆本身包括用于感测车辆周围的特征感测元件的传感器和计算设备。该计算设备包括处理单元和存储单元。存储器单元具有数据库，该数据库被配置为将周围环境中的一次性物品与可感知的特征性对象元素和可执行指令相关联。可执行指令被配置成使处理单元找到由激活的传感器感测到的环境中的任何特征感测元件与任何特征物元件之间的对应关系，基于该对应关系和设定的任务识别周围环境中的物体基于周围物体识别的参数。

2. 发明公开

EP3021076A1 SYSTEM AND METHOD FOR FLIGHT PROCEDURE CHECKING AND VERIFICATION 无效
标题翻译：系统和方法进行审查和飞行运行的确认
公开(公告)号：EP3021076A1
公开(公告)日：2016-05-18
申请号：EP14823211.9
申请日：2014-07-10
申请人： Flight Inspection Center of CAAC
发明人： SU, Wei , OUYANG, Ting , WEI, Gang , LIU, Kun , YU, Yachao , CHEN, Tao
IPC分类号： G01C11/00
CPC分类号： B64D47/08 , G01C23/00 , G08G5/0073 , G08G5/04 , G09B9/08 , G09B9/24 , G09B19/165
摘要： The present invention relates to a system and method for inspecting and validating a flight procedure used in the field of civil aviation. The system comprises an image capturing apparatus, a storage device, a playing device, a recorder such as QAR, a data processing module and a synchronization module; the method for inspecting and validating a flight procedure applied in the system includes the following steps: collecting actual visual videos and flight parameters, generating simulation visual videos, generating over-limit alarms, processing data, generating complex simulation visual videos, generating flight trajectory and flight procedure protection area pictures, and synchronizing and playing the videos. With the application of the system and the method, the defects of the prior art can be overcome, artificial sensory factors are more avoided, the general condition of an aircraft itself at each time point during the execution of the flight procedure are accurately reflected, and objective and accurate references are provided for designers and approvers of the flight procedure.

3. 发明公开

EP3403892A1 ASSESSING RUNWAY SURFACE CONDITIONS 有权
公开(公告)号：EP3403892A1
公开(公告)日：2018-11-21
申请号：EP18172326.3
申请日：2018-05-15
申请人： Goodrich Corporation
发明人： GEORGIN, Marc
IPC分类号： B60T8/17
CPC分类号： G08G5/025 , B60T8/1703 , B60T8/172 , B60T13/662 , B60W2510/069 , B60W2510/081 , B60W2510/184 , B64C25/46 , B64D45/04 , G05D1/0083 , G08G5/0021 , G08G5/0073
摘要： Systems and methods for assessing runway conditions are disclosed. The system may comprise a brake control unit (310) having an internal inertial sensor (320). The brake control unit (310) may be configured to calculate a runway coefficient of friction to assess surface conditions of the runway. The brake control unit (310) may monitor braking in an aircraft to detect a skid condition. In response to detecting the skid condition, the brake control unit (310) may calculate an aircraft deceleration of the aircraft with the inertial sensor (320). The brake control (310) unit may estimate the runway coefficient of friction based on the aircraft deceleration, an aerodynamic drag force of the aircraft, and a thrust reverse force of the aircraft (1).

4. 发明授权

EP2975595B1 SCALAR PRODUCT BASED SPACING CALCULATION 有权
标题翻译：基于标量产品的间隔计算
公开(公告)号：EP2975595B1
公开(公告)日：2018-02-21
申请号：EP15175772.1
申请日：2015-07-07
申请人： Honeywell International Inc.
发明人： KLANG, Pavel , CASEK, Petr , BRAZDILOVA, Silvie Luisa
IPC分类号： G08G5/00
CPC分类号： G08G5/0047 , G01C21/20 , G01C23/005 , G08G5/0008 , G08G5/0021 , G08G5/0026 , G08G5/0052 , G08G5/0073 , G08G5/0078 , G08G5/0082
摘要： A method is described that includes receiving, by a spacing system of an ownship aircraft, a current position of the ownship aircraft and a reference position of a target aircraft, wherein the reference position is a position of the target aircraft prior to a current position of the target aircraft. The method may also include, projecting, by the spacing system of the ownship aircraft, the reference position on a trajectory of the ownship aircraft, determining a first distance between the projected reference position and the current position, projecting, by the spacing system of the ownship aircraft, the current position on a trajectory of the reference position, determining a second distance between the projected current position and the reference position, and adjusting, by the spacing system and based on an average between the first distance and the second distance, a velocity of the ownship aircraft.

5. 发明公开

EP3170056A1 OBSTACLE AVOIDANCE SYSTEM FOR STABILIZED AERIAL VEHICLE AND METHOD OF CONTROLLING SAME 审中-公开
标题翻译：维多利亚州立大学维吾尔自治区维吾尔自治区
公开(公告)号：EP3170056A1
公开(公告)日：2017-05-24
申请号：EP14897852.1
申请日：2014-07-16
申请人： Her Majesty The Queen in Right of Canada as represented by The Minister of National Defence
发明人： WONG, Franklin , BILODEAU, Pierre Richard
IPC分类号： G05D1/10 , B64C19/00 , B64C39/02
CPC分类号： B64C39/024 , B64C19/00 , B64C2201/024 , B64C2201/027 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/203 , G05B6/02 , G05D1/0088 , G05D1/042 , G05D1/0816 , G05D1/101 , G05D1/102 , G08G5/0073 , G08G5/045
摘要： An obstacle avoidance system for a stabilized aerial vehicle and a method of controlling same are provided. Using low angular resolution obstacle proximity data, such as from low angular resolution obstacle detection sensors, when a determination is made that an operator command to a vehicle propulsion system will result in a collision, the system overrides the operator command and substitutes an avoidance speed command and avoidance heading, while maintaining operator situational awareness, in a manner that is transparent to the operator. In an implementation, examination of objects requires the obstacle avoidance system to allow the vehicle to get close to obstacles. A human-portable aerial vehicle according to an implementation can be used for building surveillance, route inspection, surveillance of windows/hallways/rooftops, power distribution towers, pipelines, bridges, buildings or close examination of suspect objects.
摘要翻译：提供了一种用于稳定的飞行器的避障系统及其控制方法。使用低角度分辨率障碍物近距离数据，例如来自低角度分辨率障碍物检测传感器，当确定对车辆推进系统的操作者命令将导致碰撞时，系统将覆盖操作员命令并代替避免速度命令并以对运营商透明的方式维护运营商的态势感知，避免航向。在实施中，物体的检查需要避障系统，使车辆靠近障碍物。根据实施的人造便携式飞行器可用于建筑物的监视，路线检查，窗户/走廊/屋顶，配电塔，管道，桥梁，建筑物的监视或可疑物体的仔细检查。

6. 发明公开

EP2993656A3 SYSTEMS AND METHODS FOR DISPLAYING OBJECT AND/OR APPROACHING VEHICLE DATA WITHIN AN AIRPORT MOVING MAP 无效转让
标题翻译：用于在机场移动地图内显示对象和/或接近机动车数据的系统和方法
公开(公告)号：EP2993656A3
公开(公告)日：2016-03-16
申请号：EP15182241.8
申请日：2015-08-24
申请人： Honeywell International Inc.
发明人： BAZAWADA, Suresh , SONGA, Anil Kumar , N, Mahesh Babu
IPC分类号： G08G5/00 , G08G5/06 , G01C21/36
CPC分类号： G08G5/065 , G01C23/00 , G08G5/0021 , G08G5/003 , G08G5/0073 , G08G5/0078 , G08G5/0086
摘要： Systems and methods for displaying object data within an airport moving map ("AMM") are disclosed. In various embodiments, the systems may comprise an avionics database, a flight management system comprising a processor communicatively coupled to the avionics database, and/or a display communicatively coupled to the processor, the processor configured to receive AMM data from the avionics database, receive object data, and/or display the AMM, the AMM including an image of the object, the AMM further including an image of an area that may be obscured from a field of view of a pilot by the object
摘要翻译：公开了用于在机场移动地图（“AMM”）内显示对象数据的系统和方法。在各种实施例中，系统可以包括航空电子设备数据库，包括通信地耦合到航空电子设备数据库的处理器的飞行管理系统，和/或通信地耦合到处理器的显示器，处理器被配置为从航空电子设备数据库接收AMM数据，对象数据和/或显示所述AMM，所述AMM包括所述对象的图像，所述AMM进一步包括可由所述对象从飞行员的视野遮蔽的区域的图像

7. 发明公开

EP3367368A1 SYSTEM AND METHOD FOR ADAPTIVE RENDERING MESSAGE REQUESTS ON A VERTICAL DISPLAY 审中-实审
公开(公告)号：EP3367368A1
公开(公告)日：2018-08-29
申请号：EP18157215.7
申请日：2018-02-16
申请人： Honeywell International Inc.
发明人： SHAMASUNDAR, Raghu , JUDD, Thomas D.
IPC分类号： G08G5/00
CPC分类号： G08G5/0021 , G06F3/04817 , G06F3/0482 , G08G5/0013 , G08G5/0026 , G08G5/0034 , G08G5/0039 , G08G5/0047 , G08G5/0073 , G08G5/045
摘要： In one embodiment, a method is provided. The method comprises: obtaining data; generating complete travel plan; determining at least one of: one or more current travel conditions and one or more future travel conditions; automatically generating at least one proposed message based upon the at least one of one or more current travel conditions and one or more future travel conditions; rendering one icon, for each of the at least one proposed message, on a grid having a first axis specifying altitude and a second axis specifying one of distance and time; and wherein each of the at least one proposed message is configured to be at least one of selectable, reviewable, printable, editable, and sendable.

8. 发明公开

EP3021076A4 SYSTEM AND METHOD FOR FLIGHT PROCEDURE CHECKING AND VERIFICATION 无效
标题翻译：联合国维吾尔族自治区ÜBERPRÜFUNGUND BESTTITIGUNG VON FLUGOPERATIONEN
公开(公告)号：EP3021076A4
公开(公告)日：2017-03-22
申请号：EP14823211
申请日：2014-07-10
申请人： FLIGHT INSPECTION CENTER OF CAAC
发明人： SU WEI , OUYANG TING , WEI GANG , LIU KUN , YU YACHAO , CHEN TAO
IPC分类号： G09B9/08 , G01C23/00 , G09B9/24
CPC分类号： B64D47/08 , G01C23/00 , G08G5/0073 , G08G5/04 , G09B9/08 , G09B9/24 , G09B19/165
摘要： The present invention relates to a system and method for inspecting and validating a flight procedure used in the field of civil aviation. The system comprises an image capturing apparatus, a storage device, a playing device, a recorder such as QAR, a data processing module and a synchronization module; the method for inspecting and validating a flight procedure applied in the system includes the following steps: collecting actual visual videos and flight parameters, generating simulation visual videos, generating over-limit alarms, processing data, generating complex simulation visual videos, generating flight trajectory and flight procedure protection area pictures, and synchronizing and playing the videos. With the application of the system and the method, the defects of the prior art can be overcome, artificial sensory factors are more avoided, the general condition of an aircraft itself at each time point during the execution of the flight procedure are accurately reflected, and objective and accurate references are provided for designers and approvers of the flight procedure.
摘要翻译：本发明涉及一种用于检查和验证在民航领域使用的飞行程序的系统和方法。该系统包括图像捕获装置，存储装置，播放装置，诸如QAR的记录器，数据处理模块和同步模块; 系统应用的飞行程序的检查和验证方法包括以下步骤：收集实际的视频和飞行参数，生成模拟视频视频，产生超限报警，处理数据，生成复杂的模拟视频视频，生成飞行轨迹和飞行程序保护区图片，以及同步和播放视频。随着系统和方法的应用，可以克服现有技术的缺陷，更加避免了人为的感官因素，飞行器本身在执行飞行过程的每个时间点的一般状况被准确地反映出来，为飞行程序的设计者和审批者提供客观准确的参考。

9. 发明公开

EP2887338A1 Ground obstacle collision alert deactivation 有权转让
标题翻译： Deaktivierung des Bodenhindernis-Kollisionsalarms
公开(公告)号：EP2887338A1
公开(公告)日：2015-06-24
申请号：EP14193962.9
申请日：2014-11-19
申请人： Honeywell International Inc.
发明人： Conner, Kevin J. , Marczi, Tomas , Haissig, Christine Marie , Glover, John Howard
IPC分类号： G08G5/06
CPC分类号： G08G5/0021 , G08G5/0073 , G08G5/06 , G08G5/065
摘要： 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.
摘要翻译：在一些示例中，处理器被配置为响应于确定飞行器处于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成响应于确定所述飞机在所述指定地面之外，来控制所述地面障碍物碰撞警报系统以自动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行器的地理位置，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。

10. 发明公开

EP3392152A1 METHOD AND SYSTEM FOR AIRCRAFT TAXI STRIKE ALERTING 有权
公开(公告)号：EP3392152A1
公开(公告)日：2018-10-24
申请号：EP18167332.8
申请日：2018-04-13
申请人： Rosemount Aerospace Inc.
发明人： RUTKIEWICZ, Robert , PESIK, Joseph T. , ELL, Todd Anthony
IPC分类号： B64D45/00 , B64F1/00 , G08G5/00 , G08G5/04 , B64D47/02 , G06K9/00 , G08G5/06
CPC分类号： G08G5/04 , B64D45/00 , B64D47/02 , B64D47/08 , B64F1/002 , G01B11/25 , G01S17/026 , G01S17/48 , G01S17/89 , G01S17/936 , G06K9/00805 , G06K9/2027 , G06K9/2036 , G06K2209/401 , G06T7/521 , G06T2207/10016 , G06T2207/10028 , G06T2207/30261 , G08G5/0021 , G08G5/0073 , G08G5/045 , G08G5/065 , H04N5/2256 , H04N5/33
摘要： Apparatus and associated methods relate to ranging object(s) (54) nearby an aircraft (12) using triangulation of pulses of linearly-patterned light projected upon and reflected by the object(s) (54). A light projector (28) projects the pulses of linearly-patterned light in a controllable direction onto the scene external to the aircraft (12). A reflected portion of the projected pulses is focused onto a selected row or column of light-sensitive pixels of a two-dimensional array, thereby forming a row or column of image data (541, 581). The direction of projected light and the row or column of pixels selected are coordinated so that the portion of the projected pulses reflected by the scene is received by the camera (30) and focused on the selected one of the rows or columns of light-sensitive pixels. Location(s) and/or range(s) of object(s) (54) in the scene are calculated, based on a projector location, a camera location, and the row or column of image data (541, 581).

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