发明名称 POWER MANAGEMENT SCHEME FOR PROTECTING COMPONENTS MOUNTED ON SPACECRAFT
摘要 <P>PROBLEM TO BE SOLVED: To provide a power management scheme for addressing problems of conventional power management schemes which can only limit the instantaneous maximum power and are not useable in a beam forming environment. <P>SOLUTION: A system for protecting a power unit 118 on a spacecraft 106 includes a ground station 108. The ground station 108 includes a power unit loading estimation and monitoring module 130 for estimating a power loading level on the power unit 118 of the spacecraft 106. The ground station 108 also includes a power regulator 128 to regulate the power of a signal for transmission from the ground station 108 to the spacecraft 106 to prevent overloading the power unit 118 of the spacecraft 106. The power of the signal for transmission to the spacecraft 106 is regulated based at least in part on an estimated power loading level on the power unit 118 of the spacecraft 106. <P>COPYRIGHT: (C)2012,JPO&INPIT
申请公布号 JP2012124900(A) 申请公布日期 2012.06.28
申请号 JP20110266422 申请日期 2011.12.06
申请人 BOEING CO:THE 发明人 WANG WEIZHENG W;BRUCE A TOMEY;SITI STEVEN F
分类号 H04B1/04;B64G1/66;H04B7/185 主分类号 H04B1/04
代理机构 代理人
主权项
地址