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11. 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。

12. 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。

13. 发明公开

EP3166093A1 AIRCRAFT SYSTEMS AND METHODS FOR PROVIDING LANDING APPROACH ALERTS 有权
标题翻译：用于提供着陆进场警报的飞机系统和方法
公开(公告)号：EP3166093A1
公开(公告)日：2017-05-10
申请号：EP16195385.6
申请日：2016-10-24
申请人： Honeywell International Inc.
发明人： ISHIHARA, Yasuo , JOHNSON, Steve
IPC分类号： G08G5/00 , G01S1/02 , G01S13/91 , G08G5/02
CPC分类号： G08G5/025 , G01S1/02 , G01S1/022 , G01S1/08 , G01S13/913 , G08G5/0021 , G08G5/0026 , G08G5/0073
摘要： A method is provided for monitoring a landing approach of an aircraft. The method includes receiving instrument landing system (ILS) signals; determining a glideslope deviation from the ILS signals; disabling, when the glideslope deviation is less than a first predetermined threshold, at least one glideslope alert function; evaluating a current glideslope condition by comparing a designated glideslope angle to a glideslope check value; and re-enabling the at least one glideslope alert function when the glideslope check value differs from the designated glideslope angle by more than a second predetermined threshold.
摘要翻译：提供了一种用于监视飞机的着陆进场的方法。该方法包括接收仪表着陆系统（ILS）信号; 确定与ILS信号的下滑角偏差; 当下坡偏差小于第一预定阈值时，禁用至少一个下滑道报警功能; 通过将指定的下滑角与下滑检查值进行比较来评估当前的下滑条件; 以及当下滑检查值与指定的下滑角相差超过第二预定阈值时重新启用至少一个下滑道警报功能。

14. 发明公开

EP2975595A3 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：EP2975595A3
公开(公告)日：2016-06-29
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.
摘要翻译：描述了一种方法，该方法包括通过本籍飞机的间隔系统接收本籍飞机的当前位置和目标飞机的基准位置，其中基准位置是目标飞机在当前位置之前的位置目标飞机。该方法还可以包括由本籍飞机的间隔系统投影本籍飞机的轨迹上的基准位置，确定投影的基准位置与当前位置之间的第一距离，本机位置在参考位置的轨迹上，确定投影的当前位置和参考位置之间的第二距离，以及通过间隔系统并基于第一距离和第二距离之间的平均值来调整本机的速度。

15. 发明公开

EP2993656A2 SYSTEMS AND METHODS FOR DISPLAYING OBJECT AND/OR APPROACHING VEHICLE DATA WITHIN AN AIRPORT MOVING MAP 无效转让
标题翻译：系统和方法的对象来显示数据和/或接近的车辆内的机场移动的卡
公开(公告)号：EP2993656A2
公开(公告)日：2016-03-09
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
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：对于机场移动地图（“AMM”）内显示的对象数据的系统和方法游离缺失光盘。在各种实施例中，系统可以包括航空电子数据库，一个飞行管理系统，包括通信地耦合到所述航空电子数据库的处理器，和/或通信地耦合到所述处理器的显示器，用于接收从所述航空电子数据库AMM数据处理器，接收对象数据，和/或显示AMM中，AMM包括对象的图像，所述AMM还包括的区域的图像也可以被从一个导频的一个场由对象遮挡

16. 发明公开

EP2975595A2 SCALAR PRODUCT BASED SPACING CALCULATION 有权
标题翻译： ABSTANDSBERECHNUNG AUF BASIS EINES SKALAREN PRODUKTS
公开(公告)号：EP2975595A2
公开(公告)日：2016-01-20
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.
摘要翻译：描述了一种方法，其包括通过本国飞行器的间隔系统接收本国飞行器的当前位置和目标飞行器的参考位置，其中参考位置是目标飞行器在当前位置之前的位置目标飞机。该方法还可以包括通过本国飞行器的间隔系统投射在本船飞行器的轨迹上的参考位置，确定投影的基准位置与当前位置之间的第一距离，确定当前位置与参考位置的轨迹之间的距离，确定投影当前位置与参考位置之间的第二距离，并且通过间隔系统和基于第一距离和第二距离之间的平均值进行调整，自身飞机的速度。

17. 发明公开

EP2902744A1 Measuring system 有权
标题翻译： Messsystem
公开(公告)号：EP2902744A1
公开(公告)日：2015-08-05
申请号：EP15151179.7
申请日：2015-01-14
申请人： Kabushiki Kaisha Topcon
发明人： Ohtomo, Fumio , Kumagai, Kaoru , Osaragi, Kazuki , Otani, Hitoshi
IPC分类号： G01C15/00
CPC分类号： G08G5/0073 , G01C15/002 , G01S19/13 , G05D1/0011 , G05D1/0094 , G08G5/0069
摘要： The invention provides a measuring system comprising a remotely controllable flying vehicle system with a GPS device and a measuring device installed thereon, a position measuring device installed at an arbitrary position and able to measure distance and angle and to track, a ground base station for controlling a flight of a flying vehicle, a remote controller able to give and take data to and from the ground base station and able to perform wireless communication to and from the flying vehicle system, and a control unit provided on the flying vehicle system or the ground base station, wherein the flying vehicle system has a retro-reflector as an object to be measured and the position measuring device is constructed so as to track the retro-reflector and perform distance measurement and angle measurement, wherein the flying vehicle system obtains GPS coordinates by the GPS device at least at two points during flight, the position measuring device measures positions of the two points of the flying vehicle system from an installation point, wherein the position measuring device measures positions of the flying vehicle system at the two points from the installation points, and either one of the control units are configured so as to obtain an absolute coordinate or GPS coordinate of the installation point of the position measuring device based on the GPS coordinates of the two points and based on distance measurement results and on angle measurement results by the position measuring device.
摘要翻译：本发明提供了一种测量系统，其包括具有GPS装置和安装在其上的测量装置的可遥控飞行系统，位置测量装置安装在任意位置并且能够测量距离和角度并跟踪地面基站用于控制飞行飞行器的飞行器，能够向和从地面基站提供数据并能够从飞行系统执行无线通信的遥控器以及设置在飞行系统或地面上的控制单元基站，其中所述飞行器系统具有作为待测对象的后向反射器，并且所述位置测量装置被构造成跟踪所述后向反射器并进行距离测量和角度测量，其中所述飞行系统获得GPS坐标由GPS装置至少在飞行中的两点处，位置测量装置测量两点的位置来自安装点的飞行系统，其中所述位置测量装置测量所述飞行系统在距所述安装点的两点处的位置，并且所述控制单元中的任一个被配置为获得所述飞行系统的绝对坐标或GPS坐标位置测量装置的安装点基于两点的GPS坐标，并基于距离测量结果和位置测量装置的角度测量结果。

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