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17 条记录 (耗时 0.03 秒)

    Method for generation of comprehensive airspace weather condition display from shared aircraft sensor data
    1.
    发明公开
    Method for generation of comprehensive airspace weather condition display from shared aircraft sensor data 有权
    一种用于产生从公共飞行器传感器数据的综合空气空间天气状况显示方法

    公开(公告)号：EP2157453A3

    公开(公告)日：2016-06-29

    申请号：EP09168016.5

    申请日：2009-08-17

    申请人： Honeywell International Inc.

    发明人： Kirk, James C.

    IPC分类号： G01W1/04 ,  G01W1/08

    CPC分类号： G01W1/08 ,  G01W1/04

    摘要： Systems and methods communicate sensor data pertaining to detected weather between aircraft. An exemplary system has at least one sensor on a transmitting aircraft (318, 320, 322), wherein the sensor is configured to detect weather and configured to output sensor data. The system has a first transceiver (212) on the transmitting aircraft (318, 320, 322) that is configured to transmit a signal with the sensor data. And the system has a second transceiver (212) on a receiving aircraft (304) that is configured to receive the signal containing the sensor data transmitted by the first transceiver (212). The sensor data of the transmitting aircraft (318, 320, 322) is fused with sensor data of the receiving aircraft (304) for a geographic region of interest to extend the effective sensor coverage and to resolve at least one of a location conflict and a severity conflict between the sensor data of the transmitting aircraft (318, 320, 322) and the receiving aircraft (304).

    Method for generation of comprehensive airspace weather condition display from shared aircraft sensor data by a receiving aircraft
    3.
    发明公开
    Method for generation of comprehensive airspace weather condition display from shared aircraft sensor data by a receiving aircraft 审中-公开
    一种用于产生从一个接收飞机的普通飞行器传感器数据的综合空气空间天气状况显示方法

    公开(公告)号：EP2157454A2

    公开(公告)日：2010-02-24

    申请号：EP09168017.3

    申请日：2009-08-17

    申请人： Honeywell International Inc.

    发明人： Kirk, James C.

    IPC分类号： G01W1/04 ,  G01W1/08

    CPC分类号： G01W1/04 ,  G01S7/003 ,  G01S13/951 ,  G01S13/953 ,  G01W1/08 ,  Y02A90/18

    摘要： Systems and methods communicate sensor data pertaining to detected weather between aircraft. An exemplary system receives a signal from a remote aircraft (318, 320, 322) that includes at least sensor data acquired from sensors on the remote aircraft (318, 320, 322). The system fuses the sensor data of the remote aircraft (318, 320, 322) with sensor data of the receiving aircraft (304) to resolve at least one of a location conflict and a severity conflict between the sensor data of the remote aircraft (318, 320, 322) and the receiving aircraft (304). The system presents weather information on a display (218) corresponding to the fused sensor data of the remote aircraft (318, 320, 322) and the receiving aircraft (304).

    摘要翻译： 系统和方法传达sensorData有关飞机之间检测到的天气。 的示例性系统从远程飞机（318，320，322）包括至少没有从sensorData传感器获取远程飞机（318，320，322）上接收的信号。 该系统融合远程飞机（318，320，322）与所述接收飞机（304）的传感器数据来解决位置冲突中的至少一个和所述远程飞机的传感器数据之间的严重程度冲突的传感器数据（318 ，320，322）和所述接收飞机（304）。 系统呈现对应于所述远程飞机（318，320，322）和所述接收飞机（304）的稠合的传感器数据的显示器（218）上的天气信息。

    Systems and methods for performing wingtip protection
    6.
    发明公开
    Systems and methods for performing wingtip protection 审中-公开
    Systeme und Verfahren zurDurchführungvonFlügelspitzenschutz

    公开(公告)号：EP2713181A1

    公开(公告)日：2014-04-02

    申请号：EP13184623.0

    申请日：2013-09-16

    申请人： Honeywell International Inc.

    发明人： Kirk, James C. ,  Bui, Long ,  Vacanti, David C. ,  Freeman, Catherine L.

    IPC分类号： G01S13/93 ,  G08G5/04

    CPC分类号： G08G5/045 ,  B64D43/00 ,  G01S13/93 ,  G01S13/931 ,  G01S2013/9335 ,  G01S2013/9339 ,  G08G5/065

    摘要： In some examples, a device or system is configured to create a narrow vertical pathway of detection that permits the enforcement of a fixed "exclusion zone" that is narrow and does not widen with range. An example system located on a vehicle includes at least two vertically separated antennas that receive radar reflection signals, a processor, and an output device. The processor receives the radar reflection signals received by the antennas, determines vertical position of any obstacles identified in the radar reflection signals and determines if the obstacles are within a predefined alert zone. The output device can output an alert if any obstacle is within the alert zone. The predefined alert zone may be related to a protruding portion of the vehicle.

    摘要翻译： 在一些示例中，设备或系统被配置为创建狭窄的垂直检测路径，其允许执行窄范围并且不随范围扩大的固定“禁区”。 位于车辆上的示例系统包括接收雷达反射信号的至少两个垂直分离的天线，处理器和输出设备。 处理器接收由天线接收的雷达反射信号，确定在雷达反射信号中识别的任何障碍物的垂直位置，并确定障碍物是否在预定警报区域内。 如果任何障碍物在警报区域内，输出设备可以输出警报。 预定警报区域可以与车辆的突出部分有关。

    Target locator device and methods
    7.
    发明公开
    Target locator device and methods 审中-公开
    Ziellokalisierungsvorrichtung und Verfahren

    公开(公告)号：EP2354752A1

    公开(公告)日：2011-08-10

    申请号：EP11152152.2

    申请日：2011-01-25

    申请人： Honeywell International Inc.

    发明人： Hartman, Randolph G. ,  Jeerage, Mahesh K. ,  Lindquist, Erik ,  Soehren, Wayne A. ,  Kirk, James C.

    IPC分类号： F41G3/02 ,  F41G3/06 ,  G01S17/02 ,  G01C19/38 ,  G01S7/497

    CPC分类号： F41G3/02 ,  F41G3/06 ,  G01C19/38 ,  G01C21/165 ,  G01C25/005 ,  G01S7/4972 ,  G01S17/023

    摘要： Systems and methods for a target locator device are provided. In one embodiment, a target locator device comprises: a high performance gyroscope; an inertial measurement unit including an accelerometer triad and a gyroscope triad; a rangefinder; a global navigation satellite system (GNSS) receiver; and a processor coupled to the high performance gyroscope, the inertial measurement unit, the rangefinder and the GNSS receiver. The processor derives an alignment heading from a heading measurement provided by the high performance gyroscope. The processor calculates a heading to a target based on a deviation from the alignment heading as measured from a heading and elevation measurement determined from the inertial measurement unit.

    摘要翻译： 提供了目标定位器设备的系统和方法。 在一个实施例中，目标定位装置包括：高性能陀螺仪; 包括加速度计三元组和陀螺仪三元组的惯性测量单元; 测距仪 全球导航卫星系统（GNSS）接收机; 以及耦合到高性能陀螺仪，惯性测量单元，测距仪和GNSS接收器的处理器。 处理器从高性能陀螺仪提供的航向测量中导出对准航向。 处理器基于从惯性测量单元确定的航向和仰角测量中测量的基于与对准航向的偏差来计算到目标的航向。