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    Terminal Area Alert System
    72.
    发明申请
    Terminal Area Alert System 审中-公开
    终端区警报系统

    公开(公告)号：US20160335899A1

    公开(公告)日：2016-11-17

    申请号：US14709890

    申请日：2015-05-12

    Applicant: The Boeing Company

    Inventor： Samantha A. Schwartz ,  Andreas Sindlinger

    IPC: G08G5/00 ,  G08G5/04

    CPC classification number: G08G5/0013 ,  G08G5/0026 ,  G08G5/0082 ,  G08G5/025

    Abstract: A method and system for handling a missed approach of an aircraft. A group of signals that indicates a go-around maneuver occurring during an approach of the aircraft to land at an airport is detected on a data bus in the aircraft. An alert to an air traffic control system for the airport when the signal is detected. The alert indicates an occurrence of the go-around maneuver, enabling rerouting of air traffic in a manner that enhances safety.

    Abstract translation: 一种用于处理飞机错过的方法和系统。 在飞机上的数据总线上检测到一组信号，指示飞机在机场降落期间发生的复飞机动。 当检测到信号时，向机场的空中交通管制系统发出警报。 该警报表示复飞机动的发生，使得能够以增强安全性的方式重新路由空中交通。

    Airspace deconfliction system and method
    73.
    发明授权
    Airspace deconfliction system and method 有权
    空域解密系统及方法

    公开(公告)号：US09495877B2

    公开(公告)日：2016-11-15

    申请号：US14287854

    申请日：2014-05-27

    Applicant: The Boeing Company

    Inventor： Michael J. Duffy ,  John J. Mattero

    IPC: G08G5/04 ,  G05D1/00 ,  G08G5/00

    CPC classification number: G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/0052 ,  G08G5/006 ,  G08G5/0069 ,  G08G5/0082

    Abstract: An aircraft deconfliction system including a registration system having an airspace database, a registered airspace, wherein registration details of the registered airspace are logged in the airspace database, and an aircraft assigned to the registered airspace, the aircraft including a flight control system, a guidance computer controlling the flight control system based on a pilot input, and an override unit in communication with the guidance computer, wherein the override unit overrides the pilot input when the aircraft breaches the registered airspace.

    Abstract translation: 一种包括具有空域数据库的注册系统的飞机解密系统，注册的空域，其中注册的空域的登记细节被记录在空域数据库中，以及分配给注册的空域的飞机，飞机包括飞行控制系统，指导 基于导频输入控制飞行控制系统的计算机以及与引导计算机通信的超控单元，其中当飞机违反注册的空域时，超控单元覆盖导频输入。

    IDENTIFYING UNMANNED AERIAL VEHICLES FOR MISSION PERFORMANCE
    78.
    发明申请
    IDENTIFYING UNMANNED AERIAL VEHICLES FOR MISSION PERFORMANCE 有权
    识别不必要的空中客车用于履行任务

    公开(公告)号：US20160247404A1

    公开(公告)日：2016-08-25

    申请号：US14282179

    申请日：2014-05-20

    Applicant: Verizon Patent and Licensing Inc.

    Inventor： Ashok N. SRIVASTAVA ,  Douglas M. PASKO ,  Hani BATLA ,  Igor KANTOR ,  Gurpreet UBHI

    IPC: G08G5/00 ,  G05D1/00 ,  G07C5/00 ,  B64C39/02

    CPC classification number: G05D1/0027 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/126 ,  B64C2201/143 ,  B64C2201/146 ,  G01C21/20 ,  G05D1/104 ,  G06Q10/047 ,  G07C5/008 ,  G08G5/0034 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/0082 ,  G08G5/0091

    Abstract: A device receives a request for a mission that includes traversal of a flight path from a first location to a second location and performance of mission operations, and calculates the flight path from the first location to the second location based on the request. The device determines required capabilities for the mission based on the request, and identifies UAVs based on the required capabilities for the mission. The device generates flight path instructions for the flight path and mission instructions for the mission operations, and provides the flight path/mission instructions to the identified UAVs to permit the identified UAVs to travel from the first location to the second location, via the flight path, and to perform the mission operations at the second location.

    Abstract translation: 设备接收对包括从第一位置到第二位置的飞行路径的遍历以及任务操作的执行的任务请求，并且基于该请求计算从第一位置到第二位置的飞行路径。 该设备根据请求确定任务所需的功能，并根据任务所需的功能识别无人机。 该设备为飞行路线生成飞行路径指令和任务操作的任务指令，并且向所识别的UAV提供飞行路线/任务指令，以允许所识别的UAV经由飞行路径从第一位置行进到第二位置 并在第二个位置执行任务操作。

    SYSTEM FOR MONITORING A-SMGCS IN REAL-TIME
    79.
    发明申请
    SYSTEM FOR MONITORING A-SMGCS IN REAL-TIME 审中-公开
    用于实时监控A-SMGCS的系统

    公开(公告)号：US20160225266A1

    公开(公告)日：2016-08-04

    申请号：US15014295

    申请日：2016-02-03

    Applicant: LSIS CO., LTD.

    Inventor： Ho-young Kang ,  Seok-Chan Lee ,  Tae-Weon Kim

    IPC: G08G5/00 ,  G08G5/06

    CPC classification number: G08G5/065 ,  G01S2013/916 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/0043 ,  G08G5/0082

    Abstract: The present disclosure relates to a monitoring technique for an Advanced-Surface Movement Guidance and Control Systeni (A-SMGCS) in real time. In the system for monitoring the A-SMGCS, which comprises the A-SMGCS and a high-level device for monitoring the A-SMGCS, an A-SMGCS server includes a monitoring module and a plurality of information transmit modules, each of which has its own status information and action information, and the monitoring module receives status information and action information sent from the plurality of information transmit modules and transmits them to the high-level device in real time.

    Abstract translation: 本公开涉及实时高级地面运动引导和控制系统（A-SMGCS）的监视技术。 在用于监视包括A-SMGCS的A-SMGCS和用于监视A-SMGCS的高级设备的A-SMGCS系统中，A-SMGCS服务器包括监控模块和多个信息发送模块，每个模块具有 其状态信息和动作信息，监视模块接收从多个信息发送模块发送的状态信息和动作信息，并将其发送到高级装置。

    Scalar product based spacing calculation
    80.
    发明授权
    Scalar product based spacing calculation 有权
    基于标量产品的间距计算

    公开(公告)号：US09384667B2

    公开(公告)日：2016-07-05

    申请号：US14334332

    申请日：2014-07-17

    Applicant: Honeywell International Inc.

    Inventor： Pavel Klang ,  Petr Casek ,  Silvie Luisa Brazdilova

    IPC: G08G5/00 ,  G01C21/20 ,  G01G23/00 ,  G01C23/00

    CPC classification number: G08G5/0047 ,  G01C21/20 ,  G01C23/005 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/0052 ,  G08G5/0073 ,  G08G5/0078 ,  G08G5/0082

    Abstract: 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.

    Abstract translation: 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来投影在自身飞行器的轨迹上的参考位置，确定投影的基准位置和当前位置之间的第一距离， 确定当前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，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。

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