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公开(公告)号：WO2016033323A1
公开(公告)日：2016-03-03
申请号：PCT/US2015/047178
申请日：2015-08-27
发明人： BJORKMAN, Marc Ronald , LANCASTER, Kim Thomas , MCKINNON, Douglas V. , ROZARIO, Novellone , TEIXEIRA, Jason Michael
IPC分类号： H04L25/03
CPC分类号： H04L27/01 , H03F1/0205 , H03F1/0266 , H03F1/0272 , H03F1/30 , H03F1/3241 , H03F1/3247 , H03F1/3276 , H03F3/19 , H03F3/195 , H03F3/211 , H03F3/245 , H03F2200/102 , H03F2200/105 , H03F2200/204 , H03F2200/405 , H03F2200/447 , H03F2200/451 , H03F2200/465 , H03F2200/468 , H03F2203/21127 , H04L25/03343 , H04L27/368 , H04L2025/03401
摘要： An adaptive linearizer system includes an adaptive linearizer circuit that is configured to pre-distort an input signal based on one or more control signals to generate a pre-distorted signal, and a non-linear high-power amplifier (HPA) having non-linear characteristics that is coupled to the adaptive linearizer circuit. The nonlinear HPA amplifies the pre-distorted signal. The pre-distortion characteristics of the adaptive linearizer circuit provide for countering the non-linear characteristics of the non-linear HPA and compensating a non-linearity of the non-linear HPA.
摘要翻译： 自适应线性化系统包括自适应线性化电路，其被配置为基于一个或多个控制信号对输入信号进行预失真以产生预失真信号，以及具有非线性的非线性高功率放大器（HPA） 耦合到自适应线性化电路的特性。 非线性HPA放大预失真信号。 自适应线性化电路的预失真特性提供了抵抗非线性HPA的非线性特性并补偿非线性HPA的非线性。
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公开(公告)号：WO2015035299A1
公开(公告)日：2015-03-12
申请号：PCT/US2014/054543
申请日：2014-09-08
IPC分类号： B64G1/50
摘要： An instrument mounting system for a geosynchronous host satellite provides independent heat rejection capability for a hosted instrument. The system may include an instrument mounting structure that is thermally coupled to a radiator component via heat pipes that may include one or both of rigid and flexible elements. In some embodiments, the system is mounted on the hosting satellite so as to provide satellite components and the hosted instrument with a clear field of view while rejecting heat in one or both of the north and south directions. The system may also provide structural support for components of one or both of the hosted instrument or the hosting satellite.
摘要翻译： 用于地球同步主机卫星的仪器安装系统为托管仪器提供独立的散热能力。 该系统可以包括通过可以包括刚性和柔性元件中的一个或两者的热管热耦合到散热器部件的仪器安装结构。 在一些实施例中，系统被安装在主机卫星上，以便在卫星组件和托管的仪器中提供清晰的视场，同时在北向和南方的一个或两个方向上排除热量。 该系统还可以为托管的仪器或托管卫星中的一个或两个的组件提供结构支持。
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公开(公告)号：WO2021207345A1
公开(公告)日：2021-10-14
申请号：PCT/US2021/026155
申请日：2021-04-07
摘要： A panel assembly for use with a spacecraft includes a payload, a radiator panel and a heat pipe. The payload is configured to generate waste heat during operation. The radiator panel is spaced apart from the payload and is configured to dissipate waste heat. The heat pipe is coupled to the payload and the radiator panel. The heat pipe includes a compliant portion to permit the radiator panel to move relative to the payload. Further the heat pipe is configured to transfer waste heat from the payload to the radiator panel.
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公开(公告)号：WO2016029190A1
公开(公告)日：2016-02-25
申请号：PCT/US2015/046424
申请日：2015-08-21
发明人： BJORKMAN, Marc Ronald , LANCASTER, Kim Thomas , MCKINNON, Douglas V. , ROZARIO, Novellone , TEIXEIRA, Jason Michael
IPC分类号： H03F1/32
CPC分类号： H04B7/1851 , H03F1/3241 , H03F1/3276 , H03F3/195 , H03F3/245 , H03F2200/405 , H03F2200/451 , H04B1/0475 , H04B2001/0425
摘要： A high-linearity linearizer system includes a multi-stage linearizer circuit formed by cascading multiple linearizer circuits. The multi-stage linearizer circuit is configured to pre-distort an input signal to generate a pre-distorted signal. A non-linear high-power amplifier (HPA) having non-linear characteristics is coupled to the multi-stage linearizer circuit and is configured to amplify the pre-distorted signal. Pre-distortion characteristics of the multi-stage linearizer circuit are configured to counter the non-linear characteristics of the non-linear HPA and to compensate a non-linearity of the non-linear HPA to achieve a desired level of linearity.
摘要翻译： 高线性线性化系统包括通过级联多个线性化电路而形成的多级线性化电路。 多级线性化电路被配置为对输入信号进行预失真以产生预失真信号。 具有非线性特性的非线性高功率放大器（HPA）耦合到多级线性化电路，并被配置为放大预失真信号。 多级线性化电路的预失真特性被配置为对抗非线性HPA的非线性特性并且补偿非线性HPA的非线性以实现期望的线性水平。
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5.发明申请
公开(公告)号：WO2014022312A1
公开(公告)日：2014-02-06
申请号：PCT/US2013/052575
申请日：2013-07-29
摘要： An apparatus for satellite communication may include a reflector configured to redirect electromagnetic energy. Each of multiple feeds may be positioned at a predetermined location with respect to the reflector. A feed-switching mechanism may be configured to selectively activate for use at least one of the multiple feeds. A steering mechanism may be configured to steer the reflector such that a focal point of the reflector approximately coincides with a position of an activated feed of the multiple feeds. The reflector may be mechanically independent of the plurality of feeds and the feed-switching mechanism.
摘要翻译： 用于卫星通信的装置可以包括被配置为重定向电磁能的反射器。 多个进料中的每一个可以相对于反射器定位在预定位置。 馈送切换机构可以被配置为选择性地激活以使用多个馈送中的至少一个。 转向机构可以被配置成转向反射器，使得反射器的焦点大致与多个进给器的激活进给的位置重合。 反射器可以机械地独立于多个进料和进料切换机构。
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公开(公告)号：WO2007109380A2
公开(公告)日：2007-09-27
申请号：PCT/US2007/060501
申请日：2007-01-12
IPC分类号： B64G1/52
摘要： A satellite (50) is disclosed having at least one deployable thermal radiator (64). Once deployed, this thermal radiator (64) may be repositioned. In one embodiment, the deployed thermal radiator (64) may be moved about a first axis (74), about a second axis (76), or both to move the deployed thermal radiator (64) from one deployed position to another deployed position.
摘要翻译： 公开了一种具有至少一个可展开散热器（64）的卫星（50）。 一旦部署，该热散热器（64）可以重新定位。 在一个实施例中，部署的热辐射器（64）可围绕第一轴线（74）绕第二轴线（76）或两者移动，以将部署的散热器（64）从一个展开位置移动到另一展开位置。
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