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    • 5. 发明授权
    • ODU alignment procedure using circularly polarized signals allocated to specific satellites
    • 使用分配给特定卫星的圆偏振信号的ODU对准程序
    • US08044872B2
    • 2011-10-25
    • US11971808
    • 2008-01-09
    • Gustave R. StroesBenjamin Mui
    • Gustave R. StroesBenjamin Mui
    • H01Q3/00
    • H01Q1/1257H01Q3/06H01Q19/12H01Q25/007
    • A method and system for aligning an antenna reflector with satellites in a satellite configuration. A method in accordance with the present invention comprises pointing the reflector to an orbital slot used in the satellite configuration, wherein only one satellite in the orbital slot transmits first circularly polarized signals, and adjusting the reflector to maximize reception of the first circularly polarized signals from the orbital slot. A system in accordance with the present invention comprises a reflector, a power meter coupled to the reflector, wherein the power meter and reflector are tuned to receive first circularly polarized signals, and an alignment mechanism, coupled to the reflector, wherein the alignment mechanism is manipulated to point the reflector at an orbital slot wherein only one satellite in the orbital slot transmits the first circularly polarized signals, and to adjust the reflector to maximize reception of the first circularly polarized signals from the orbital slot.
    • 一种用于将天线反射器与卫星配置中的卫星对准的方法和系统。 根据本发明的方法包括将反射器指向卫星配置中使用的轨道槽,其中轨道槽中仅一个卫星发射第一圆偏振信号,并且调整反射器以最大限度地接收第一圆偏振信号 轨道槽。 根据本发明的系统包括反射器,耦合到反射器的功率计,其中调谐功率计和反射器以接收第一圆偏振信号,以及耦合到反射器的对准机构,其中对准机构是 被操纵以将反射器指向轨道槽,其中轨道槽中仅一个卫星传输第一圆偏振信号,并且调整反射器以最大限度地从轨道槽接收第一圆偏振信号。
    • 7. 发明授权
    • ODU alignment procedure using circularly polarized squint
    • ODU校正程序使用圆偏振眯
    • US07978142B2
    • 2011-07-12
    • US11971800
    • 2008-01-09
    • Gustave R. StroesBenjamin Mui
    • Gustave R. StroesBenjamin Mui
    • H01Q3/00
    • H01Q1/1257H01Q3/06H01Q19/12H01Q25/007
    • A method and system for aligning an antenna reflector with satellites in a satellite configuration. A method in accordance with the present invention comprises coarsely pointing the reflector to an orbital slot used in the satellite configuration, wherein at least one satellite in the orbital slot transmits first circularly polarized signals, and adjusting the reflector to maximize reception of the first circularly polarized signals from the orbital slot. A system in accordance with the present invention comprises a reflector, a power meter coupled to the reflector, wherein the power meter and reflector are tuned to receive first circularly polarized signals, and an alignment mechanism, coupled to the reflector, wherein the alignment mechanism is manipulated to point the reflector at an orbital slot wherein at least one satellite in the orbital slot transmits the first circularly polarized signals, and to adjust the reflector to maximize reception of the first circularly polarized signals from the orbital slot.
    • 一种用于将天线反射器与卫星配置中的卫星对准的方法和系统。 根据本发明的方法包括将反射器粗略地指向在卫星配置中使用的轨道槽,其中轨道槽中的至少一个卫星传输第一圆偏振信号,并且调整反射器以最大化接收第一圆偏振 来自轨道槽的信号。 根据本发明的系统包括反射器,耦合到反射器的功率计,其中调谐功率计和反射器以接收第一圆偏振信号,以及耦合到反射器的对准机构,其中对准机构是 操纵以将反射器指向轨道槽,其中轨道槽中的至少一个卫星传输第一圆偏振信号,并且调整反射器以最大化地从轨道槽接收第一圆偏振信号。
    • 8. 发明申请
    • ODU ALIGNMENT PROCEDURE USING CIRCULARLY POLARIZED SIGNALS ALLOCATED TO SPECIFIC SATELLITES
    • 使用分配给特定卫星的通用极化信号的ODU对准程序
    • US20080165070A1
    • 2008-07-10
    • US11971808
    • 2008-01-09
    • Gustave R. StroesBenjamin Mui
    • Gustave R. StroesBenjamin Mui
    • H01Q3/00
    • H01Q1/1257H01Q3/06H01Q19/12H01Q25/007
    • A method and system for aligning an antenna reflector with satellites in a satellite configuration. A method in accordance with the present invention comprises pointing the reflector to an orbital slot used in the satellite configuration, wherein only one satellite in the orbital slot transmits first circularly polarized signals, and adjusting the reflector to maximize reception of the first circularly polarized signals from the orbital slot. A system in accordance with the present invention comprises a reflector, a power meter coupled to the reflector, wherein the power meter and reflector are tuned to receive first circularly polarized signals, and an alignment mechanism, coupled to the reflector, wherein the alignment mechanism is manipulated to point the reflector at an orbital slot wherein only one satellite in the orbital slot transmits the first circularly polarized signals, and to adjust the reflector to maximize reception of the first circularly polarized signals from the orbital slot.
    • 一种用于将天线反射器与卫星配置中的卫星对准的方法和系统。 根据本发明的方法包括将反射器指向卫星配置中使用的轨道槽,其中轨道槽中仅一个卫星发射第一圆偏振信号,并且调整反射器以最大限度地接收第一圆偏振信号 轨道槽。 根据本发明的系统包括反射器,耦合到反射器的功率计,其中调谐功率计和反射器以接收第一圆偏振信号,以及耦合到反射器的对准机构,其中对准机构是 被操纵以将反射器指向轨道槽,其中轨道槽中仅一个卫星传输第一圆偏振信号,并且调整反射器以最大限度地从轨道槽接收第一圆偏振信号。
    • 9. 发明申请
    • ODU ALIGNMENT PROCEDURE USING CIRCULARLY POLARIZED SQUINT
    • ODU对齐程序使用圆形极化SQUINT
    • US20080165069A1
    • 2008-07-10
    • US11971800
    • 2008-01-09
    • Gustave R. StroesBenjamin Mui
    • Gustave R. StroesBenjamin Mui
    • H01Q3/00
    • H01Q1/1257H01Q3/06H01Q19/12H01Q25/007
    • A method and system for aligning an antenna reflector with satellites in a satellite configuration. A method in accordance with the present invention comprises coarsely pointing the reflector to an orbital slot used in the satellite configuration, wherein at least one satellite in the orbital slot transmits first circularly polarized signals, and adjusting the reflector to maximize reception of the first circularly polarized signals from the orbital slot. A system in accordance with the present invention comprises a reflector, a power meter coupled to the reflector, wherein the power meter and reflector are tuned to receive first circularly polarized signals, and an alignment mechanism, coupled to the reflector, wherein the alignment mechanism is manipulated to point the reflector at an orbital slot wherein at least one satellite in the orbital slot transmits the first circularly polarized signals, and to adjust the reflector to maximize reception of the first circularly polarized signals from the orbital slot.
    • 一种用于将天线反射器与卫星配置中的卫星对准的方法和系统。 根据本发明的方法包括将反射器粗略地指向在卫星配置中使用的轨道槽,其中轨道槽中的至少一个卫星传输第一圆偏振信号,并且调整反射器以最大化接收第一圆偏振 来自轨道槽的信号。 根据本发明的系统包括反射器,耦合到反射器的功率计,其中调谐功率计和反射器以接收第一圆偏振信号,以及耦合到反射器的对准机构,其中对准机构是 操纵以将反射器指向轨道槽,其中轨道槽中的至少一个卫星传输第一圆偏振信号,并且调整反射器以最大化地从轨道槽接收第一圆偏振信号。