发明名称 Method and apparatus for establishing a reference potential on satellites in planetary ionospheres
摘要 A simple, nearly passive apparatus is disclosed that allows a spacecraft sensor to be driven to a potential close to that of a plasma where the ion concentration exceeds about 100 cm-3 even in the presence of a large vehicle potential. The apparatus includes a conductive reference surface insulated from all spacecraft elements. The reference surface is situated on the spacecraft such that it faces in the direction of motion, and collects ions thereon. There is developed on the surface a plasma potential. The reference surface is connected to the inverting input of an operational amplifier that is powered by floating voltages referenced to the potential at the noninverting input of the amplifier. Since the operational amplifier has to maintain equal voltages at both inputs, the amplifier will drive against spacecraft ground until the voltage at the noninverting input is substantially equal to the voltage at the inverting input. The reference potential established at the noninverting input is therefore the same as the potential on the reference surface.
申请公布号 US4576348(A) 申请公布日期 1986.03.18
申请号 US19830508470 申请日期 1983.06.28
申请人 BOARD OF REGENTS, UNIVERSITY OF TEXAS SYSTEM 发明人 ZUCCARO, DON R.
分类号 B64G1/44;B64G1/54;(IPC1-7):B64G1/54;H01G1/08 主分类号 B64G1/44
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