Parameter analysis of PAF for whole-spacecraft vibration isolation

DOI10.1016/J.AST.2007.02.006zbMATH Open1195.74075OpenAlexW2055605778MaRDI QIDQ4929552

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Publication date: 23 September 2010

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ast.2007.02.006

zbMATH Keywords

spacecraftvibration isolationwhole-spacecraft vibration isolationpayload attach Fitting

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Finite element methods applied to problems in solid mechanics (74S05)

Related Items (2)

Disturbance and vibration isolation in space stations by means of mechanical decoupling ⋮ Design and experiment of micro-vibration isolation system for optical satellite

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