2018 IEEE Aerospace Conference 2018
DOI: 10.1109/aero.2018.8396415
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Design and evaluation of an end-effector for a reconfigurable multi-robot system for future planetary missions

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Cited by 3 publications
(1 citation statement)
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“…Within the last few millimeters of the locking stroke, the locking device pushes the tapered surface of the locking probe head to complete the EMI locking process. 60,71,72 It is worth noting that the EMI is considered to reduce the impact of the surface dust during the docking process. The specific design for the EMI interface includes optimization configuration on the guide pin, improvement of the connection method for the electrical connector with tab electrical connection interface, as well as addition of a dust-proof baffle for the locking mechanism.…”
Section: Mechanical Docking Interfacesmentioning
confidence: 99%
“…Within the last few millimeters of the locking stroke, the locking device pushes the tapered surface of the locking probe head to complete the EMI locking process. 60,71,72 It is worth noting that the EMI is considered to reduce the impact of the surface dust during the docking process. The specific design for the EMI interface includes optimization configuration on the guide pin, improvement of the connection method for the electrical connector with tab electrical connection interface, as well as addition of a dust-proof baffle for the locking mechanism.…”
Section: Mechanical Docking Interfacesmentioning
confidence: 99%