Conceptual design of deployable solar array inspired by Miura origami
This paper dedicates on a conceptual design of origami inspired solar arrays.The requirements of novel solar arrays for future spacecrafts are firstly discussed,followed by a summary of origami applied in industry,especially on deployable solar arrays.The conclusion that origami is a preferred solution has been obtained.Comparisons between origami patterns lead to a Miura-inspired scheme.A system design including panels,deployable mechanism,and hold-down and release mechanism has been implemented.The kinematics and dynamic analyses have been carried out so that the feasibility of Miura-inspired solar array has been verified.A detailed design will be accomplished,and a prototype will be established for ground validation,followed by iterative optimizations in the next stage.
deployable solar array Miura origami
Ming Li Zhiyi Wang Qifeng Cui Yan Chen Feizhou Shi Jiayao Ma Jian Gao Wenbin Xu Hantian Zhong Wei Yuan
Space Structure and Mechanism Technology Laboratory of China Aerospace Science and Technology Group Motion Structures Laboratory,Tianjin University,Tianjin 300354,China
国内会议
北京
英文
250-255
2018-08-02（万方平台首次上网日期，不代表论文的发表时间）