发明名称 Force feedback refueling system for unmanned aircraft
摘要 An in-flight refueling system for an unmanned aircraft is responsive to sensed forces acting on a refueling receptacle of the aircraft by a separate refueling probe, to control movements of the aircraft as it is being refueled to reduce the magnitude of the sensed forces and thereby maintain the coupling of the aircraft with the refueling probe.
申请公布号 US7021586(B2) 申请公布日期 2006.04.04
申请号 US20040782253 申请日期 2004.02.19
申请人 THE BOEING COMPANY 发明人 BOLLING JOHN G.
分类号 B64C1/00;B64C39/02;B64D39/00 主分类号 B64C1/00
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