发明名称 Method for deploying an orbiting sparse array antenna
摘要 A deployment method maintains a cluster of subsatellites within a rigid formation relative to and orbiting about a real or fictitious center satellite that in turn orbits the earth in a frozen inclined eccentric reference orbit by determining the subsatellite reference orbits of the each of the subsatellites based upon position and velocity vectors of the center satellite. The determined subsatellite reference orbits can then be maintained through fuel efficient microthrusting so as to maintain the rigid formation for coherently combining communication signals within a very large sparse antenna array formed by the cluster having improved beam directionality for improved signal communications.
申请公布号 US6725012(B1) 申请公布日期 2004.04.20
申请号 US20000495731 申请日期 2000.02.01
申请人 THE AEROSPACE CORPORATION 发明人 JANSON SIEGFRIED W.;POLLARD JAMES E.;CHAO CHIA-CHUN
分类号 B64G1/10;B64G1/24;(IPC1-7):H04B7/185;G06E7/00 主分类号 B64G1/10
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