-
1.发明授权Integrated antenna and RF payload for low-cost inter-satellite links using super-elliptical antenna aperture with single axis gimbal 有权集成天线和RF有效载荷，用于使用单轴万向节的超椭圆天线孔径的低成本卫星间链路公开(公告)号：US09590299B2
公开(公告)日：2017-03-07
申请号：US14739540
申请日：2015-06-15
Applicant: NORTHROP GRUMMAN SYSTEMS CORPORATION
Inventor： Sudhakar K. Rao , Daniel H. Roper , Alan M. Taft , Sebong Chun , Christopher S. Brown , Mansoor K. Siddique
CPC classification number: H01Q3/20 , H01Q1/288 , H01Q3/06 , H01Q19/132 , H01Q19/134 , H01Q19/193
Abstract: A dual-reflector inter-satellite link (ISL) subsystem, for a communications satellite in a constellation of satellites in low earth orbit or medium earth orbit. The ISL subsystem includes a main antenna reflector which uses a single-axis gimbal to steer the main reflector only in the elevation plane. An antenna subreflector, a horn and RF feed circuitry are stationary with respect to the host satellite. The main reflector has a super-elliptical design which provides a beam shape which requires no steering in the azimuth plane, while meeting ISL signal strength requirements. By steering the main reflector only, and only in the elevation plane, the disclosed ISL subsystem delivers significantly lower size, mass, complexity and cost, and significantly greater reliability, than traditional ISL systems.
Abstract translation: 用于低地球轨道或中等轨道卫星星座中的通信卫星的双反射器卫星间链路（ISL）子系统。 ISL子系统包括主天线反射器，其使用单轴万向架仅在仰角平面中引导主反射器。 天线子反射器，喇叭和RF馈电电路相对于主卫星是固定的。 主反射器具有超椭圆形设计，其提供了在方位平面中不需要转向的梁形状，同时满足ISL信号强度要求。 通过仅转向主反射器，仅在高程平面上，与传统的ISL系统相比，所公开的ISL子系统显着降低了尺寸，质量，复杂性和成本，并显着提高了可靠性。
-
2.发明申请INTEGRATED ANTENNA AND RF PAYLOAD FOR LOW-COST INTER-SATELLITE LINKS USING SUPER-ELLIPTICAL ANTENNA APERTURE WITH SINGLE AXIS GIMBAL 有权集成天线和射频PAYLOAD用于低成本的卫星间链路使用超级天线孔与单轴GIMBAL公开(公告)号：US20160365630A1
公开(公告)日：2016-12-15
申请号：US14739540
申请日：2015-06-15
Applicant: NORTHROP GRUMMAN SYSTEMS CORPORATION
Inventor： SUDHAKAR K. RAO , Daniel H. Roper , Alan M. Taft , Sebong Chun , Christopher S. Brown , Mansoor K. Siddique
CPC classification number: H01Q3/20 , H01Q1/288 , H01Q3/06 , H01Q19/132 , H01Q19/134 , H01Q19/193
Abstract: A dual-reflector inter-satellite link (ISL) subsystem, for a communications satellite in a constellation of satellites in low earth orbit or medium earth orbit, is disclosed. The ISL subsystem includes a main antenna reflector which uses a single-axis gimbal to steer the main reflector only in the elevation plane. An antenna subreflector, a horn and RF feed circuitry are stationary with respect to the host satellite. The main reflector has a super-elliptical design which provides a beam shape which requires no steering in the azimuth plane, while meeting ISL signal strength requirements. By steering the main reflector only, and only in the elevation plane, the disclosed ISL subsystem delivers significantly lower size, mass, complexity and cost, and significantly greater reliability, than traditional ISL systems.
Abstract translation: 公开了一种用于低地球轨道或中等轨道卫星星座中的通信卫星的双反射器卫星间链路（ISL）子系统。 ISL子系统包括主天线反射器，其使用单轴万向架仅在仰角平面中引导主反射器。 天线子反射器，喇叭和RF馈电电路相对于主卫星是固定的。 主反射器具有超椭圆形设计，其提供了在方位平面中不需要转向的梁形状，同时满足ISL信号强度要求。 通过仅转向主反射器，仅在高程平面上，与传统的ISL系统相比，所公开的ISL子系统显着降低了尺寸，质量，复杂性和成本，并显着提高了可靠性。
-
Search Results
2
records
(took 0.012 seconds)
