发明名称 MISSILE GUIDANCE SYSTEM
摘要 In a CLOS missile guidance system, target and missile tracking data e.g. video image data are acquired on a UAV and transmitted to the missile where they are processed to provide guidance control data to the missile. Alternatively the video image data may be transmitted to a command station where the guidance control data is generated and transmitted to the missile, preferably via the UAV.
申请公布号 US2011084161(A1) 申请公布日期 2011.04.14
申请号 US20100672443 申请日期 2010.01.08
申请人 MBDA UK LIMITED 发明人 WALLIS GRAHAM PATRICK
分类号 F41G7/30 主分类号 F41G7/30
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