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Frontiers of Mechanical Engineering >> 2024, Volume 19, Issue 3 doi: 10.1007/s11465-024-0789-z
A novel stiffness optimization model of space telescopic boom based on locking mechanism
1. School of Mechanical Engineering and Automation, Beihang University, Beijing 100191, China;1. School of Mechanical Engineering and Automation, Beihang University, Beijing 100191, China;2. Beijing Institute of Spacecraft System Engineering, Beijing 100094, China;1. School of Mechanical Engineering and Automation, Beihang University, Beijing 100191, China;2. Beijing Institute of Spacecraft System Engineering, Beijing 100094, China;2. Beijing Institute of Spacecraft System Engineering, Beijing 100094, China;1. School of Mechanical Engineering and Automation, Beihang University, Beijing 100191, China;1. School of Mechanical Engineering and Automation, Beihang University, Beijing 100191, China
Abstract
Keywords
deployable telescopic boom ; locking mechanism ; stiffness model ; clearance error ; optimization model
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