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公开(公告)号：US08786506B2
公开(公告)日：2014-07-22
申请号：US13278927
申请日：2011-10-21
申请人： Keith Ayotte , Paul Lagasse , David Martin , Anthony Sorrentino , Spencer Webb , Mark Wheeler , George Davison
发明人： Keith Ayotte , Paul Lagasse , David Martin , Anthony Sorrentino , Spencer Webb , Mark Wheeler , George Davison
IPC分类号： H01Q3/00
CPC分类号： H01Q1/08 , H01Q1/1235 , H01Q1/125 , H01Q3/005
摘要： A low power, lightweight, collapsible and rugged antenna positioner for use in communicating with geostationary, geosynchronous and low earth orbit satellite. By collapsing, invention may be easily carried or shipped in a compact container. May be used in remote locations with simple or automated setup and orientation. Azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. Manual orientation of antenna for linear polarized satellites yields lower weight and power usage. Updates ephemeris or TLE data via satellite. Algorithms used for search including Clarke Belt fallback, transponder/beacon searching switch, azimuth priority searching and tracking including uneven re-peak scheduling yield lower power usage. Orientation aid via user interface allows for smaller azimuth motor, simplifies wiring and lowers weight. Tilt compensation, bump detection and failure contingency provide robustness.
摘要翻译： 低功率，轻量级，可折叠和坚固的天线定位器，用于与地球静止，地球同步和低地球轨道卫星通信。 通过塌缩，发明可以容易地携带或运输在紧凑的容器中。 可以在远程位置使用简单或自动的设置和方向。 通过相对于定位器基座旋转天线来调节方位角，并通过旋转与天线耦合的升降马达来调节高度。 用于线性极化卫星的手动定向天线产生较小的重量和功率使用。 通过卫星更新星历或TLE数据。 用于搜索的算法包括克拉克带回退，转发器/信标搜索开关，方位优先搜索和跟踪，包括不均匀的重峰调度产生较低的功率使用。 通过用户界面定向辅助，可以实现更小的方位电机，简化接线和降低重量。 倾斜补偿，碰撞检测和故障应急提供了鲁棒性。
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公开(公告)号：US20120068899A1
公开(公告)日：2012-03-22
申请号：US13278927
申请日：2011-10-21
申请人： Keith AYOTTE , Paul Lagasse , David Martin , Anthony Sorrentino , Mark Wheeler , Spencer Webb , George Davison
发明人： Keith AYOTTE , Paul Lagasse , David Martin , Anthony Sorrentino , Mark Wheeler , Spencer Webb , George Davison
IPC分类号： H01Q3/00
CPC分类号： H01Q1/08 , H01Q1/1235 , H01Q1/125 , H01Q3/005
摘要： A low power, lightweight, collapsible and rugged antenna positioner for use in communicating with geostationary, geosynchronous and low earth orbit satellite. By collapsing, invention may be easily carried or shipped in a compact container. May be used in remote locations with simple or automated setup and orientation. Azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. Manual orientation of antenna for linear polarized satellites yields lower weight and power usage. Updates ephemeris or TLE data via satellite. Algorithms used for search including Clarke Belt fallback, transponder/beacon searching switch, azimuth priority searching and tracking including uneven re-peak scheduling yield lower power usage. Orientation aid via user interface allows for smaller azimuth motor, simplifies wiring and lowers weight. Tilt compensation, bump detection and failure contingency provide robustness.
摘要翻译： 低功率，轻量级，可折叠和坚固的天线定位器，用于与地球静止，地球同步和低地球轨道卫星通信。 通过塌缩，发明可以容易地携带或运输在紧凑的容器中。 可以在远程位置使用简单或自动的设置和方向。 通过相对于定位器基座旋转天线来调节方位角，并通过旋转与天线耦合的升降马达来调节高度。 用于线性极化卫星的手动定向天线产生较小的重量和功率使用。 通过卫星更新星历或TLE数据。 用于搜索的算法包括克拉克带回退，转发器/信标搜索开关，方位优先搜索和跟踪，包括不均匀的重峰调度产生较低的功率使用。 通过用户界面定向辅助，可以实现更小的方位电机，简化接线和降低重量。 倾斜补偿，碰撞检测和故障应急提供了鲁棒性。
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公开(公告)号：US07889144B2
公开(公告)日：2011-02-15
申请号：US12236149
申请日：2008-09-23
申请人： Spencer Webb , David Martin
发明人： Spencer Webb , David Martin
IPC分类号： H01Q3/00
摘要： A low power, lightweight, collapsible and rugged antenna positioner for use in communicating with geostationary, geosynchronous and low earth orbit satellite. By collapsing, invention may be easily carried or shipped in a compact container. May be used in remote locations with simple or automated setup and orientation. Azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. Manual orientation of antenna for linear polarized satellites yields lower weight and power usage. Updates ephemeris or TLE data via satellite. Algorithms used for search including Clarke Belt fallback, transponder/beacon searching switch, azimuth priority searching and tracking including uneven re-peak scheduling yield lower power usage. Orientation aid via user interface allows for smaller azimuth motor, simplifies wiring and lowers weight. Tilt compensation, bump detection and failure contingency provide robustness.
摘要翻译： 低功率，轻量级，可折叠和坚固的天线定位器，用于与地球静止，地球同步和低地球轨道卫星通信。 通过塌缩，发明可以容易地携带或运输在紧凑的容器中。 可以在远程位置使用简单或自动的设置和方向。 通过相对于定位器基座旋转天线来调节方位角，并通过旋转与天线耦合的升降马达来调节高度。 用于线性极化卫星的手动定向天线产生较小的重量和功率使用。 通过卫星更新星历或TLE数据。 用于搜索的算法包括克拉克带回退，转发器/信标搜索开关，方位优先搜索和跟踪，包括不均匀的重峰调度产生较低的功率使用。 通过用户界面定向辅助，可以实现更小的方位电机，简化接线和降低重量。 倾斜补偿，碰撞检测和故障应急提供了鲁棒性。
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公开(公告)号：US20090021438A1
公开(公告)日：2009-01-22
申请号：US12236149
申请日：2008-09-23
申请人： Spencer Webb , David Martin
发明人： Spencer Webb , David Martin
IPC分类号： H01Q3/00
摘要： A low power, lightweight, collapsible and rugged antenna positioner for use in communicating with geostationary, geosynchronous and low earth orbit satellite. By collapsing, invention may be easily carried or shipped in a compact container. May be used in remote locations with simple or automated setup and orientation. Azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. Manual orientation of antenna for linear polarized satellites yields lower weight and power usage. Updates ephemeris or TLE data via satellite. Algorithms used for search including Clarke Belt fallback, transponder/beacon searching switch, azimuth priority searching and tracking including uneven re-peak scheduling yield lower power usage. Orientation aid via user interface allows for smaller azimuth motor, simplifies wiring and lowers weight. Tilt compensation, bump detection and failure contingency provide robustness.
摘要翻译： 低功率，轻量级，可折叠和坚固的天线定位器，用于与地球静止，地球同步和低地球轨道卫星通信。 通过塌缩，发明可以容易地携带或运输在紧凑的容器中。 可以在远程位置使用简单或自动的设置和方向。 通过相对于定位器基座旋转天线来调节方位角，并通过旋转与天线耦合的升降马达来调节高度。 用于线性极化卫星的手动定向天线产生较小的重量和功率使用。 通过卫星更新星历或TLE数据。 用于搜索的算法包括克拉克带回退，转发器/信标搜索开关，方位优先搜索和跟踪，包括不均匀的重峰调度产生较低的功率使用。 通过用户界面定向辅助，可以实现更小的方位电机，简化接线和降低重量。 倾斜补偿，碰撞检测和故障应急提供了鲁棒性。
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公开(公告)号：US20050248498A1
公开(公告)日：2005-11-10
申请号：US11115960
申请日：2005-04-26
申请人： Spencer Webb , David Martin
发明人： Spencer Webb , David Martin
摘要： Embodiments of the portable antenna positioner described provide a lightweight, collapsible and rugged antenna positioner for use in receiving low earth orbit, geostationary and geosynchronous satellite transmissions. By collapsing the antenna positioner, it may be readily carried by one person or shipped in a compact container. The antenna positioner may be used in remote locations with simple or automated setup and orientation. In order to operate the apparatus, azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. The apparatus may update ephemeris data via satellite, may comprise a built-in receiver and may couple with a second positioner base comprising cryptographic, router or power functionality. The apparatus may comprise storage devices such as a hard drive or flash disk for storing data to and from at least one satellite.
摘要翻译： 所描述的便携式天线定位器的实施例提供了一种用于接收低地球轨道，对地静止和地球同步卫星传输的轻量级，可折叠和坚固的天线定位器。 通过折叠天线定位器，它可以容易地由一个人承载或运送在紧凑的容器中。 天线定位器可以在远程位置使用，具有简单或自动的设置和方向。 为了操作该装置，通过相对于定位器基座旋转天线来调节方位角，并且通过旋转与天线耦合的升降马达来调节高度。 该装置可以通过卫星更新星历数据，可以包括内置的接收机，并且可以与包括密码，路由器或电源功能的第二定位器基座耦合。 该装置可以包括诸如硬盘驱动器或闪存盘的存储设备，用于将数据存储到和从至少一个卫星存储。
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公开(公告)号：US07173571B2
公开(公告)日：2007-02-06
申请号：US11115960
申请日：2005-04-26
申请人： Spencer Webb , David Martin
发明人： Spencer Webb , David Martin
IPC分类号： H01Q3/00
摘要： Embodiments of the portable antenna positioner described provide a lightweight, collapsible and rugged antenna positioner for use in receiving low earth orbit, geostationary and geosynchronous satellite transmissions. By collapsing the antenna positioner, it may be readily carried by one person or shipped in a compact container. The antenna positioner may be used in remote locations with simple or automated setup and orientation. In order to operate the apparatus, azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. The apparatus may update ephemeris data via satellite, may comprise a built-in receiver and may couple with a second positioner base comprising cryptographic, router or power functionality. The apparatus may comprise storage devices such as a hard drive or flash disk for storing data to and from at least one satellite.
摘要翻译： 所描述的便携式天线定位器的实施例提供了用于接收低地球轨道，对地静止和地球同步卫星传输的轻量级，可折叠和坚固的天线定位器。 通过折叠天线定位器，它可以容易地由一个人承载或运送在紧凑的容器中。 天线定位器可以在远程位置使用，具有简单或自动的设置和方向。 为了操作该装置，通过相对于定位器基座旋转天线来调节方位角，并且通过旋转与天线耦合的升降马达来调节高度。 该装置可以通过卫星更新星历数据，可以包括内置的接收机，并且可以与包括密码，路由器或电源功能的第二定位器基座耦合。 该装置可以包括诸如硬盘驱动器或闪存盘的存储设备，用于将数据存储到和从至少一个卫星存储。
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公开(公告)号：US20070001920A1
公开(公告)日：2007-01-04
申请号：US11412720
申请日：2006-04-26
申请人： Spencer Webb , David Martin
发明人： Spencer Webb , David Martin
IPC分类号： H01Q3/00
摘要： A low power, lightweight, collapsible and rugged antenna positioner for use in communicating with geostationary, geosynchronous and low earth orbit satellite. By collapsing, invention may be easily carried or shipped in a compact container. May be used in remote locations with simple or automated setup and orientation. Azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. Manual orientation of antenna for linear polarized satellites yields lower weight and power usage. Updates ephemeris or TLE data via satellite. Algorithms used for search including Clarke Belt fallback, transponder/beacon searching switch, azimuth priority searching and tracking including uneven re-peak scheduling yield lower power usage. Orientation aid via user interface allows for smaller azimuth motor, simplifies wiring and lowers weight. Tilt compensation, bump detection and failure contingency provide robustness.
摘要翻译： 低功率，轻量级，可折叠和坚固的天线定位器，用于与地球静止，地球同步和低地球轨道卫星通信。 通过塌缩，发明可以容易地携带或运输在紧凑的容器中。 可以在远程位置使用简单或自动的设置和方向。 通过相对于定位器基座旋转天线来调节方位角，并通过旋转与天线耦合的升降马达来调节高度。 用于线性极化卫星的手动定向天线产生较小的重量和功率使用。 通过卫星更新星历或TLE数据。 用于搜索的算法包括克拉克带回退，转发器/信标搜索开关，方位优先搜索和跟踪，包括不均匀的重峰调度产生较低的功率使用。 通过用户界面定向辅助，可以实现更小的方位电机，简化接线和降低重量。 倾斜补偿，碰撞检测和故障应急提供了鲁棒性。
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公开(公告)号：US08068062B2
公开(公告)日：2011-11-29
申请号：US12986891
申请日：2011-01-07
申请人： Spencer Webb , David Martin
发明人： Spencer Webb , David Martin
IPC分类号： H01Q3/00
摘要： A low power, lightweight, collapsible and rugged antenna positioner for use in communicating with geostationary, geosynchronous and low earth orbit satellite. By collapsing, invention may be easily carried or shipped in a compact container. May be used in remote locations with simple or automated setup and orientation. Azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. Manual orientation of antenna for linear polarized satellites yields lower weight and power usage. Updates ephemeris or TLE data via satellite. Algorithms used for search including Clarke Belt fallback, transponder/beacon searching switch, azimuth priority searching and tracking including uneven re-peak scheduling yield lower power usage. Orientation aid via user interface allows for smaller azimuth motor, simplifies wiring and lowers weight. Tilt compensation, bump detection and failure contingency provide robustness.
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公开(公告)号：US07432868B2
公开(公告)日：2008-10-07
申请号：US11412720
申请日：2006-04-26
申请人： Spencer Webb , David Martin
发明人： Spencer Webb , David Martin
IPC分类号： H01Q3/00
摘要： A low power, lightweight, collapsible and rugged antenna positioner for use in communicating with geostationary, geosynchronous and low earth orbit satellite. By collapsing, invention may be easily carried or shipped in a compact container. May be used in remote locations with simple or automated setup and orientation. Azimuth is adjusted by rotating an antenna in relation to a positioner base and elevation is adjusted by rotating an elevation motor coupled with the antenna. Manual orientation of antenna for linear polarized satellites yields lower weight and power usage. Updates ephemeris or TLE data via satellite. Algorithms used for search including Clarke Belt fallback, transponder/beacon searching switch, azimuth priority searching and tracking including uneven re-peak scheduling yield lower power usage. Orientation aid via user interface allows for smaller azimuth motor, simplifies wiring and lowers weight. Tilt compensation, bump detection and failure contingency provide robustness.
摘要翻译： 低功率，轻量级，可折叠和坚固的天线定位器，用于与地球静止，地球同步和低地球轨道卫星通信。 通过塌缩，发明可以容易地携带或运输在紧凑的容器中。 可以在远程位置使用简单或自动的设置和方向。 通过相对于定位器基座旋转天线来调节方位角，并通过旋转与天线耦合的升降马达来调节高度。 用于线性极化卫星的手动定向天线产生较小的重量和功率使用。 通过卫星更新星历或TLE数据。 用于搜索的算法包括克拉克带回退，转发器/信标搜索开关，方位优先搜索和跟踪，包括不均匀的重峰调度产生较低的功率使用。 通过用户界面定向辅助，可以实现更小的方位电机，简化接线和降低重量。 倾斜补偿，碰撞检测和故障应急提供了鲁棒性。
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10.发明申请COMPACT RADIO FREQUENCY TRANSMITTING AND RECEIVING ANTENNA AND CONTROL DEVICE EMPLOYING SAME 有权紧凑无线电频率发射和接收天线及其使用的控制装置公开(公告)号：US20080036679A1
公开(公告)日：2008-02-14
申请号：US11874642
申请日：2007-10-18
申请人： Spencer Webb , Stephen Thompson , Gregory Altonen , Stuart DeJonge , Edward Felegy , Siddharth Sinha
发明人： Spencer Webb , Stephen Thompson , Gregory Altonen , Stuart DeJonge , Edward Felegy , Siddharth Sinha
IPC分类号： H01Q7/00
摘要： An electrical control device for controlling the status of a controlled electrical device, the electrical control device comprising a power conducting semiconductor device for controlling the status of the controlled electrical device; a control circuit; a transmitter and/or receiver in communication with the control circuit; and an antenna coupled to the transmitter and/or receiver; the antenna adapted to receive a first signal at a specified frequency from a remote control device and/or transmit a second signal at a specified frequency to a remote control device; wherein the transmitter is operable to couple the first signal from the antenna to the control circuit for remotely controlling the controllably conductive device and/or couple the second signal from the control circuit for providing a status of said controlled electrical device, the antenna comprising a first loop of conductive material having a capacitance and an inductance; the capacitance and the inductance forming a circuit being resonant at the specified frequency; a second loop of conductive material having two ends adapted to be electrically coupled to a control circuit, the second loop being substantially only magnetically coupled to the first loop; the first and second loops each having a loop axis, the loop axes of the first and second loops being substantially parallel or coincident.
摘要翻译： 一种用于控制受控电气设备的状态的电气控制装置，所述电气控制装置包括用于控制受控电气装置的状态的功率传导半导体装置; 一个控制电路; 与控制电路通信的发射机和/或接收机; 以及耦合到所述发射机和/或接收机的天线; 所述天线适于从遥控设备接收指定频率的第一信号和/或以指定频率发送到遥控设备的第二信号; 其中所述发射机可操作以将来自所述天线的所述第一信号耦合到所述控制电路，以远程控制所述可控导电装置和/或耦合来自所述控制电路的所述第二信号，以提供所述受控电气装置的状态，所述天线包括第一 具有电容和电感的导电材料的环路; 形成电路的电容和电感以指定频率谐振; 导电材料的第二环，其具有适于电耦合到控制电路的两端，所述第二环基本上仅磁耦合到所述第一环; 所述第一和第二回路各自具有回转轴线，所述第一和第二回路的回转轴基本上平行或重合。
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