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    • 1. 发明申请
    • DISTRIBUTED AND CABLE REDUCED TCAS
    • 分布式和电缆减少TCAS
    • US20080068250A1
    • 2008-03-20
    • US11748848
    • 2007-05-15
    • Ruy C. BrandaoJames B. Jones
    • Ruy C. BrandaoJames B. Jones
    • G01S13/00
    • G01S13/9303G01S3/46G08G5/0008G08G5/0078
    • A direction finding antenna system for determining the relative bearing of a second aircraft from a first aircraft in conjunction with a Traffic Alert Collision Avoidance System (TCAS). The system includes a first antenna and a second antenna located on a top surface of the first aircraft, spaced apart along a first axis, as well as a third antenna and a fourth antenna located on a bottom surface of the first aircraft, spaced apart along a second axis orthogonal to the first axis. The system further includes a transmitting, receiving, and processing system coupled to the first, second, third, and fourth antennas, wherein the transmitting, receiving, and processing system is configured to transmit TCAS interrogations, receive TCAS replies, and process the TCAS replies to determine the relative bearing of the second aircraft from the first aircraft.
    • 一种方向发现天线系统,用于与交通警报冲突避免系统(TCAS)一起确定来自第一架飞机的第二架飞机的相对方位。 该系统包括位于第一飞行器的顶表面上的第一天线和第二天线,沿着第一轴线间隔开,以及位于第一飞行器的底表面上的第三天线和第四天线,其间隔开 与第一轴正交的第二轴。 该系统还包括耦合到第一,第二,第三和第四天线的发射,接收和处理系统,其中所述发射,接收和处理系统被配置为传输TCAS询问,接收TCAS应答并处理TCAS应答 以确定来自第一架飞机的第二架飞机的相对方位。
    • 3. 发明申请
    • SYSTEMS AND METHODS FOR PROVIDING DIVERSITY-DISTANCE-MEASURING EQUIPMENT
    • 提供多方位测量设备的系统和方法
    • US20140015707A1
    • 2014-01-16
    • US13545530
    • 2012-07-10
    • James B. JonesRuy C. Brandao
    • James B. JonesRuy C. Brandao
    • G01S13/08
    • G01S13/785
    • Systems and methods that allow for distance-measuring equipment (DME) to use either a lower or an upper fuselage-mounted antenna. An exemplary system located on an aircraft includes an aircraft configuration data source that generates aircraft configuration information, an aircraft orientation data source that generates aircraft orientation information, a positioning system that generates aircraft position information and a component that provides DME ground station position information. The system also includes a first antenna, a second antenna and a processing device that determines if a DME signal communication issue exists with the first antenna that is based on the generated aircraft position information, the DME ground station position information and at least one of the configuration or orientation information. The processing device switches DME signal communication to the second antenna if a DME signal communication issue has been determined to exist.
    • 允许距离测量设备(DME)使用下部或上部机身安装天线的系统和方法。 位于飞行器上的示例性系统包括生成飞行器配置信息的飞行器配置数据源,产生飞行器方向信息的飞行器方向数据源,产生飞行器位置信息的定位系统和提供DME地面站位置信息的组件。 该系统还包括第一天线,第二天线和处理装置,其基于所生成的飞机位置信息,DME地面站位置信息和DME地面站位置信息确定第一天线是否存在DME信号通信问题 配置或方向信息。 如果已经确定存在DME信号通信问题,则处理设备将DME信号通信切换到第二天线。
    • 5. 发明授权
    • Systems and methods for providing diversity-distance-measuring equipment
    • 用于提供分集距离测量设备的系统和方法
    • US09030348B2
    • 2015-05-12
    • US13545530
    • 2012-07-10
    • James B. JonesRuy C. Brandao
    • James B. JonesRuy C. Brandao
    • G01S13/08G01S13/78
    • G01S13/785
    • Systems and methods that allow for distance-measuring equipment (DME) to use either a lower or an upper fuselage-mounted antenna. An exemplary system located on an aircraft includes an aircraft configuration data source that generates aircraft configuration information, an aircraft orientation data source that generates aircraft orientation information, a positioning system that generates aircraft position information and a component that provides DME ground station position information. The system also includes a first antenna, a second antenna and a processing device that determines if a DME signal communication issue exists with the first antenna that is based on the generated aircraft position information, the DME ground station position information and at least one of the configuration or orientation information. The processing device switches DME signal communication to the second antenna if a DME signal communication issue has been determined to exist.
    • 允许距离测量设备(DME)使用下部或上部机身安装天线的系统和方法。 位于飞行器上的示例性系统包括生成飞行器配置信息的飞行器配置数据源,产生飞行器方向信息的飞行器方向数据源,产生飞行器位置信息的定位系统和提供DME地面站位置信息的组件。 该系统还包括第一天线,第二天线和处理装置,其基于所生成的飞机位置信息,DME地面站位置信息和DME地面站位置信息确定第一天线是否存在DME信号通信问题 配置或方向信息。 如果已经确定存在DME信号通信问题,则处理设备将DME信号通信切换到第二天线。
    • 6. 发明授权
    • Distributed and cable reduced TCAS
    • 分布式和电缆减少TCAS
    • US07978121B2
    • 2011-07-12
    • US12551295
    • 2009-08-31
    • Ruy C. BrandaoJames B. Jones
    • Ruy C. BrandaoJames B. Jones
    • G01S13/93G01S13/74
    • G01S13/9303G01S3/46G08G5/0008G08G5/0078
    • A direction finding antenna system for determining the relative bearing of a second aircraft from a first aircraft in conjunction with Distance Measuring Equipment (DME). The system includes a first antenna and a second antenna located on a top surface of the first aircraft, spaced apart along a first axis, as well as a third antenna and a fourth antenna located on a bottom surface of the first aircraft, spaced apart along a second axis orthogonal to the first axis. The system further includes a transmitting, receiving, and processing system coupled to the first, second, third, and fourth antennas, wherein the transmitting, receiving, and processing system is configured to transmit DME interrogations, receive DME replies, and process the DME replies to determine the relative bearing of the second aircraft from the first aircraft.
    • 一种测向天线系统,用于与距离测量设备(DME)一起确定来自第一架飞机的第二架飞机的相对方位。 该系统包括位于第一飞行器的顶表面上的第一天线和第二天线,沿着第一轴线间隔开,以及位于第一飞行器的底表面上的第三天线和第四天线,其间隔开 与第一轴正交的第二轴。 该系统还包括耦合到第一,第二,第三和第四天线的发射,接收和处理系统,其中,所述发射,接收和处理系统被配置为发送DME询问,接收DME响应并处理DME应答 以确定来自第一架飞机的第二架飞机的相对方位。
    • 7. 发明申请
    • DISTRIBUTED AND CABLE REDUCED TCAS
    • 分布式和电缆减少TCAS
    • US20100117886A1
    • 2010-05-13
    • US12551295
    • 2009-08-31
    • Ruy C. BrandaoJames B. Jones
    • Ruy C. BrandaoJames B. Jones
    • G01S13/93G01S13/08
    • G01S13/9303G01S3/46G08G5/0008G08G5/0078
    • A direction finding antenna system for determining the relative bearing of a second aircraft from a first aircraft in conjunction with Distance Measuring Equipment (DME). The system includes a first antenna and a second antenna located on a top surface of the first aircraft, spaced apart along a first axis, as well as a third antenna and a fourth antenna located on a bottom surface of the first aircraft, spaced apart along a second axis orthogonal to the first axis. The system further includes a transmitting, receiving, and processing system coupled to the first, second, third, and fourth antennas, wherein the transmitting, receiving, and processing system is configured to transmit DME interrogations, receive DME replies, and process the DME replies to determine the relative bearing of the second aircraft from the first aircraft.
    • 一种测向天线系统,用于与距离测量设备(DME)一起确定来自第一架飞机的第二架飞机的相对方位。 该系统包括位于第一飞行器的顶表面上的第一天线和第二天线,沿着第一轴线间隔开,以及位于第一飞行器的底表面上的第三天线和第四天线,其间隔开 与第一轴正交的第二轴。 该系统还包括耦合到第一,第二,第三和第四天线的发射,接收和处理系统,其中,所述发射,接收和处理系统被配置为发送DME询问,接收DME响应并处理DME应答 以确定来自第一架飞机的第二架飞机的相对方位。
    • 8. 发明授权
    • Distributed and Cable reduced TCAS
    • 分布式和电缆减少TCAS
    • US07583223B2
    • 2009-09-01
    • US11748848
    • 2007-05-15
    • Ruy C. BrandaoJames B. Jones
    • Ruy C. BrandaoJames B. Jones
    • G01S13/93G01S13/74
    • G01S13/9303G01S3/46G08G5/0008G08G5/0078
    • A direction finding antenna system for determining the relative bearing of a second aircraft from a first aircraft in conjunction with a Traffic Alert Collision Avoidance System (TCAS). The system includes a first antenna and a second antenna located on a top surface of the first aircraft, spaced apart along a first axis, as well as a third antenna and a fourth antenna located on a bottom surface of the first aircraft, spaced apart along a second axis orthogonal to the first axis. The system further includes a transmitting, receiving, and processing system coupled to the first, second, third, and fourth antennas, wherein the transmitting, receiving, and processing system is configured to transmit TCAS interrogations, receive TCAS replies, and process the TCAS replies to determine the relative bearing of the second aircraft from the first aircraft.
    • 一种方向发现天线系统,用于与交通警报冲突避免系统(TCAS)一起确定来自第一架飞机的第二架飞机的相对方位。 该系统包括位于第一飞行器的顶表面上的第一天线和第二天线,沿着第一轴线间隔开,以及位于第一飞行器的底表面上的第三天线和第四天线,其间隔开 与第一轴正交的第二轴。 该系统还包括耦合到第一,第二,第三和第四天线的发射,接收和处理系统,其中所述发射,接收和处理系统被配置为传输TCAS询问,接收TCAS应答并处理TCAS应答 以确定来自第一架飞机的第二架飞机的相对方位。
    • 9. 发明授权
    • Method for reducing transmit power for traffic alert and collision avoidance systems and airborne collision avoidance systems
    • 降低交通警报和防撞系统以及机载碰撞避免系统的发射功率的方法
    • US06483453B2
    • 2002-11-19
    • US09943039
    • 2001-08-29
    • David OeyRuy C. BrandaoLuAn VannessLarry D. King
    • David OeyRuy C. BrandaoLuAn VannessLarry D. King
    • G01S1300
    • G01S13/765G01S13/781G01S13/9303
    • The present invention provides a method for efficient use of the transmit power of a Traffic Alert Collision Avoidance System (TCAS) that allows enhanced surveillance range and limits radio frequency (RF) interference in crowded airspace. The method reduces power density in crowded airspace by modifying Mode S, Mode A and Mode C interrogations. During Mode S broadcasts, tracking interrogation power is reduced as a function of range. Further transmit power reduction is achieved by broadcasting a variable power density whisper-shout interrogation technique for Mode A/C aircraft when garbling is detected. If garbling is observed during a medium whisper-shout interrogation sequence, the method of the present invention attempts to clear the garbling by using focused high-density whisper-shout steps but only in the ranges where garbling was detected. Formation members can account for other formation members that are TCAS equipped using a special E-TCAS Broadcast Interrogation. The presence of other E-TCAS will be used in the RF interference limiting calculations. Aircraft flying in formation further minimize broadcast power by sharing information between the formation leader and formation aircraft.
    • 本发明提供了一种有效利用交通警报冲突避免系统(TCAS)的发射功率的方法,其允许增强的监视范围并限制拥挤的空域中的射频(RF)干扰。 该方法通过修改模式S,模式A和模式C询问来降低拥挤空域的功率密度。 在模式S广播期间,跟踪询问功率作为范围的函数减小。 当检测到乱码时,通过广播用于模式A / C飞机的可变功率密度耳语询问技术来实现进一步的发射功率降低。 如果在中等耳语询问序列期间观察到乱码,则本发明的方法尝试通过使用聚焦的高密度耳语步骤来清除乱码,但是仅在检测到乱码的范围内。 组成员可以考虑使用特殊的E-TCAS广播讯问装备TCAS的其他组织成员。 其他E-TCAS的存在将用于RF干扰限制计算。 飞机飞行通过在地层导弹和地面飞机之间共享信息进一步最小化广播能力。