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作 者:Chenyang Ji Jinguo Liu Chenchen Wu Pengyuan Zhao Keli Chen
机构地区:[1]State Key Laboratory of Robotics,Shenyang Institute of Automation,Chinese Academy of Science,Shenyang 110016,China [2]Institutes for Robotics and Intelligent Manufacturing,Chinese Academy of Sciences,Shenyang 110169,China [3]School of Mechanical Engineering and Automation,Northeastern University,Shenyang 110819,China [4]University of Chinese Academy of Sciences,Beijing 100049,China
出 处:《Chinese Journal of Mechanical Engineering》2023年第2期279-290,共12页中国机械工程学报(英文版)
基 金:Supported by National Key R&D Program of China (Grant No.2018YFB1304600);National Natural Science Foundation of China (Grant No.51905527);CAS Interdisciplinary Innovation Team of China (Grant No.JCTD-2018-11);State Key Laboratory of Robotics Foundation of China (Grant No.Y91Z0303)。
摘 要:Large-scale solar sails can provide power to spacecraft for deep space exploration.A new type of telescopic tubular mast(TTM)driven by a bistable carbon fiber-reinforced polymer tube was designed in this study to solve the problem of contact between the sail membrane and the spacecraft under light pressure.Compared with the traditional TTM,it has a small size,light weight,high extension ratio,and simple structure.The anti-blossoming and self-unlocking structure of the proposed TTM was described.We aimed to simplify the TTM with a complex structure into a beam model with equal linear mass density,and the simulation results showed good consistency.The dynamic equation was derived based on the equivalent model,and the effects of different factors on the vibration characteristics of the TTM were analyzed.The performance parameters were optimized based on a multiobjective genetic algorithm,and prototype production and load experiments were conducted.The results show that the advantages of the new TTM can complete the deployment of large-scale solar sails,which is valuable for future deep space exploration.
关 键 词:Telescopic tubular mast Solar sail Genetic algorithm Modal analysis OPTIMIZATION
分 类 号:V442[航空宇航科学与技术—飞行器设计] V414.1
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