Composite vibration control device for micro-vibration of on-orbit spacecraft

The invention relates to the technical field of spaceflight, in particular to a combined type vibration control device for micro vibration of an on-orbit spacecraft and a satellite vibration reduction system. A first fixed magnetic ring, a second fixed magnetic ring, a second pair of fixed magnetic...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ZHANG SHAN, WANG HAOYU, ZHANG YEWEI, ZANG JIAN, ZHANG ZHEN, LIU PENGPENG, XIAO RONGHUAN
Format: Patent
Sprache:chi ; eng
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