发明名称 Autonomous satellite docking system
摘要 This invention solves problems associated with prior-art soft-dock mechanisms by placing all active components of a soft-dock system on the chaser side of the mechanism, leaving the target side of the mechanism completely passive (i.e., requiring no power expenditure or self-actuated moving parts to operate). In particular, the active components are supported on the end of a flexible cable attached to the probe, or chaser, side of the device. These components act as a sort of spring-loaded "trap." Once the end of the probe passes into a receptacle on the target side, the mechanism is triggered, engaging it in such a way that it can no longer be pulled out of the receptacle until it is reset. The soft-docking cable may be replaced with a rigid, semi-rigid or jointed post that is used to bring a capture mechanism into engagement with its corresponding receptacle or receiving structure. The magnetic end effector may also be implemented as an electro-magnet, which requires power to maintain the holding force, or a permanent magnet, which captures a target without power. The metallic main target cone may be use a non-metallic cone constructed of fabric, plastic, or other flexible material.
申请公布号 US2004245405(A1) 申请公布日期 2004.12.09
申请号 US20040857808 申请日期 2004.06.01
申请人 TCHORYK PETE;PAVLICH JANE;WASSICK GREG;HAYS ANTHONY B.;RITTER GREG 发明人 TCHORYK PETE;PAVLICH JANE;WASSICK GREG;HAYS ANTHONY B.;RITTER GREG
分类号 B64G1/64;(IPC1-7):B64G1/46 主分类号 B64G1/64
代理机构 代理人
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