Methods for presenting traffic information on an aircraft display unit
    1.
    发明授权
    Methods for presenting traffic information on an aircraft display unit 有权
    在飞机显示单元上呈现交通信息的方法

    公开(公告)号:US08773288B1

    公开(公告)日:2014-07-08

    申请号:US13237209

    申请日:2011-09-20

    IPC分类号: G08B21/00

    CPC分类号: G08G5/0021 G08G5/0008

    摘要: Present novel and non-trivial methods for presenting traffic information are disclosed. In a first method, data representative of ownship position, first traffic, and second traffic are received by a traffic symbology generator (“TSG”). The traffic is divided into zones and a correlation between the targets of the traffic is determined. A traffic symbology data set is generated by the TSG based upon the results of the correlation(s). In a second method, data representative of ownship position and first traffic, runway references, and a selectable display range are received by the TSG. The traffic is divided into zones, and a traffic symbology data set is generated by the TSG thereafter. In a third method, data representative of ownship position and first traffic are received by the TSG. The traffic is divided into zones, and a traffic symbology data set is generated by the TSG thereafter.

    摘要翻译: 介绍了呈现交通信息的新颖而不平凡的方法。 在第一种方法中,由业务符号生成器(“TSG”)接收表示本地位置,第一业务和第二业务的数据。 流量被划分为区域,确定了交通目标之间的相关性。 基于相关性的结果,由TSG生成交通符号系统数据集。 在第二种方法中,由TSG接收表示本身位置和第一交通量,跑道参考和可选显示范围的数据。 流量分为区域,之后由TSG生成流量符号系统数据集。 在第三种方法中,由TSG接收表示本身位置和第一业务的数据。 流量分为区域,之后由TSG生成流量符号系统数据集。

    System, device, and method for presenting instrument approach procedure advisory information to a pilot on an aircraft
    2.
    发明授权
    System, device, and method for presenting instrument approach procedure advisory information to a pilot on an aircraft 有权
    用于向飞机上的飞行员呈现仪器进近程序咨询信息的系统,装置和方法

    公开(公告)号:US09002544B1

    公开(公告)日:2015-04-07

    申请号:US13459273

    申请日:2012-04-30

    IPC分类号: G01C23/00

    CPC分类号: G01C23/005 G01C23/00

    摘要: A present novel and non-trivial system, device, and method for presenting instrument approach procedure (“IAP”) advisory information to a pilot of an aircraft are disclosed. An advisory generator (“AG”) is programmed to retrieve or receive flight information representative of the current position of the aircraft, a designated airport, and at least one published IAP; weather minima data corresponding to each IAP; and one or more IAP suitability factors from a weather data source, a NOTAM data source, and/or an aircraft performance data source. The AG determines the suitability or availability of each published IAP, disables the pilot's selectability of each unsuitable or unavailable published IAP, and generates advisory data representative of information advising the pilot of the unsuitable or unavailable published IAP(s). Additionally, the AG is programmed to receive a pilot's override of an unsuitable or unavailable published IAP and enable the overridden unsuitable or unavailable IAP.

    摘要翻译: 公开了一种用于向飞行员的飞行员呈现仪器进近程序(“IAP”)咨询信息的现有小说和非平凡的系统,装置和方法。 一个咨询生成器(“AG”)被编程为检索或接收代表飞机,指定机场和至少一个已发布的IAP的当前位置的飞行信息; 对应于每个IAP的天气最小值数据; 以及来自天气数据源,NOTAM数据源和/或飞行器性能数据源的一个或多个IAP适合性因素。 AG确定每个已发布的IAP的适用性或可用性,禁止飞行员对每个不合适或不可用的已发布IAP的可选性,并生成咨询数据,代表不合适或不可用的已发布IAP的飞行员的信息。 此外,AG被编程为接收飞行员对不合适或不可用的已发布IAP的覆盖,并启用覆盖不适用或不可用的IAP。

    Mapping, storage, retrieval and display of high energy electromagnetic radiation emitters
    3.
    发明授权
    Mapping, storage, retrieval and display of high energy electromagnetic radiation emitters 有权
    高能电磁辐射发射器的映射,存储,检索和显示

    公开(公告)号:US08692703B1

    公开(公告)日:2014-04-08

    申请号:US12884530

    申请日:2010-09-17

    IPC分类号: G01S7/36

    CPC分类号: G01S7/36 G08G5/0034 G08G5/006

    摘要: A system for providing the capability for a vehicle to avoid regions of signal interference from high energy (HE) electromagnetic (EM) radiation emitters. The system includes a processing module. A database is operatively connected to the processing module. The database comprises a plurality of geographical areas affected by HE EM radiation emitters and data associated with the geographical areas. The data includes location, lateral and vertical extents, and signal attenuation for selected geographical areas affected by HE EM radiation emitters. The data preferably also includes affected frequency spectrum for the selected geographical areas. A display system is operatively connected to the processing module. The processing module functions to receive information regarding the position of the vehicle and query the database to retrieve relevant HE EM radiation emitters which are a threat to the vehicle's ability to properly navigate or communicate. The relevant HE EM radiation emitters are displayed on the display system. The present invention provides enhanced situational awareness to the pilot and permits decision support systems to refine their trajectory through hazards.

    摘要翻译: 一种用于提供车辆能力以避免来自高能量(HE)电磁(EM)辐射发射器的信号干扰区域的系统。 该系统包括处理模块。 数据库可操作地连接到处理模块。 数据库包括受HE EM辐射发射器影响的多个地理区域和与地理区域相关联的数据。 数据包括受HE EM辐射发射器影响的所选地理区域的位置,横向和垂直范围以及信号衰减。 数据优选地还包括所选择的地理区域的受影响的频谱。 显示系统可操作地连接到处理模块。 处理模块用于接收关于车辆位置的信息并查询数据库以检索对车辆正确导航或通信能力的威胁的相关HE EM辐射发射器。 相关的HE EM辐射发射器显示在显示系统上。 本发明为飞行员提供了增强的情境意识,并允许决策支持系统通过危险来改进其轨迹。

    System, module, and method for presenting runway advisory information to a pilot
    4.
    发明授权
    System, module, and method for presenting runway advisory information to a pilot 有权
    向飞行员介绍跑道咨询信息的系统,模块和方法

    公开(公告)号:US08193948B1

    公开(公告)日:2012-06-05

    申请号:US12570019

    申请日:2009-09-30

    IPC分类号: G08B23/00

    摘要: A present novel and non-trivial system, module, and method for presenting runway advisory information are disclosed. A runway reference may be established using data received from a source of navigation reference data, where such data could represent runway information, runway awareness zone information, landing awareness zone information, and/or runway threshold line information. Navigation data representative of at least aircraft location and input factor data may be received from a source. Phase of flight may be determined using input factor data, and a runway advisory data set may be generated as a function of phase of flight and the positional relationship between aircraft location and the runway reference. Runway advisory data set may be representative of advisory information comprised of visual runway advisory information, aural runway advisory information, tactile advisory information, or a combination thereof. A presentation system receives the runway advisory data set and presents advisory information.

    摘要翻译: 公开了一种用于呈现跑道咨询信息的现有小说和非平凡的系统,模块和方法。 可以使用从导航参考数据源接收的数据来建立跑道参考,其中这样的数据可以表示跑道信息,跑道感知区域信息,着陆感知区域信息和/或跑道阈值线信息。 可以从源接收至少代表飞机位置和输入因子数据的导航数据。 可以使用输入因子数据确定飞行阶段,并且可以产生作为飞行阶段和飞机位置与跑道参考之间的位置关系的函数的跑道咨询数据集。 跑道咨询数据集可以代表由视觉跑道咨询信息,听觉跑道咨询信息,触觉咨询信息或其组合组成的咨询信息。 演示系统接收跑道咨询数据集并呈现咨询信息。

    TCAS primary antenna on aircraft underside system and method
    5.
    发明授权
    TCAS primary antenna on aircraft underside system and method 有权
    飞机下面的TCAS主天线系统和方法

    公开(公告)号:US08976057B1

    公开(公告)日:2015-03-10

    申请号:US13540419

    申请日:2012-07-02

    申请人: Randy H. Jacobson

    发明人: Randy H. Jacobson

    IPC分类号: G01S13/93 G01S3/14 G08G5/04

    摘要: A system and method for operational placement of Traffic Collision and Avoidance System (TCAS) antennas on an aerial vehicle. A TCAS primary directional antenna is configured to mount on a lower surface of the aerial vehicle wherein the directional antenna receives and determines a direction of reception of an RF signal. The omnidirectional antenna is mounted on an upper surface of the aerial vehicle for transmission and reception of TCAS signals. A TCAS processor has associated ports to send and receive signals to each antenna for communicating with TCAS target aircraft. The TCAS processor is configured to recognize a mounted location of the antennas via signals received from the inputs. The TCAS processor is further configured to accept a plurality of inputs via the associated ports from the lower mounted directional antenna yet still output accurate TCAS information to the TCAS display.

    摘要翻译: 一种用于在航空器上运行交通碰撞和避雷系统(TCAS)天线的系统和方法。 TCAS主定向天线被配置为安装在空中交通工具的下表面上,其中定向天线接收并确定RF信号的接收方向。 全向天线安装在飞行器的上表面,用于发送和接收TCAS信号。 TCAS处理器具有相关端口,用于向每个天线发送和接收信号以与TCAS目标飞机通信。 TCAS处理器被配置为通过从输入接收的信号来识别天线的安装位置。 TCAS处理器还被配置为经由来自下安装的定向天线的相关端口接受多个输入,但仍然向TCAS显示器输出准确的TCAS信息。