发明名称 Missile tracking by GPS reflections
摘要 A system for engaging hostile air or space threats with a defensive missile, where the defensive missile comprises an antenna for receiving global positioning system (GPS) signals. A global positioning system receiver is coupled to said antenna, for receiving global positioning system signals directly from global positioning system satellites and global positioning system signals reflected from the threat. A processing arrangement processes the direct and reflected global positioning system signals for determining the position and velocity of the threat. Vectoring controls are coupled to the processing arrangement, and are responsive to the location of the threat for directing the defensive missile toward the threat. In a particular embodiment, the antenna of the defensive missile is directionally controllable, and the defensive missile includes an antenna direction controller responsive to the processor for directing at least a beam of the antenna toward the threat.
申请公布号 US8610041(B1) 申请公布日期 2013.12.17
申请号 US201113113487 申请日期 2011.05.23
申请人 BOARDMAN JONATHAN A.;LOCKHEED MARTIN CORPORATION 发明人 BOARDMAN JONATHAN A.
分类号 F41G7/22;F41G7/00;F42B15/00;F42B15/01 主分类号 F41G7/22
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