Design and dynamic simulation of hinged deployable configuration spacecraft

被引：0
|
作者：
Ma, Shangjun [1 ]
Liu, Geng [1 ]
Luo, Hao [1 ]
机构：
[1] School of Mechatronical Engineering, Northwestern Polytechnical University, Xi'an 710072, China
来源：
Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology | 2010年 / 30卷 / 06期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：49 / 56
相关论文
共 50 条
  • [21] Configuration Design and Kinematics Research of Scissor Unit Deployable Mechanism
    Li, Jianfeng
    Wang, Sanmin
    Zhi, Changjian
    Sun, Yuantao
    MECHANISM AND MACHINE SCIENCE, 2017, 408 : 749 - 759
  • [22] Design optimization of modular configuration for deployable truss antenna reflector
    Hu Fei
    Song Yanping
    Huang Zhirong
    Li Yichen
    Ma Xiaofei
    Li Wan
    CHINESE SPACE SCIENCE AND TECHNOLOGY, 2022, 42 (01) : 99 - 106
  • [23] A Methodology for Optimal Design and Simulation of Deployable Structures
    del Ama, Fernando
    Molina, Mariano
    Isabel Castilla, M.
    Gomez Pulido, Dolores
    Lorenzo, Covadonga
    Garcia Millan, Juan
    Sancho, Juan C.
    5TH WORLD MULTIDISCIPLINARY CIVIL ENGINEERING-ARCHITECTURE-URBAN PLANNING SYMPOSIUM (WMCAUS), 2020, 960
  • [24] Dynamic modeling and analysis of large axially deployable spacecraft under gravity gradient
    Sun, Tongtong
    Zhang, Shuo
    Du, Lin
    Dong, Hao
    Zhao, Yunping
    Deng, Zichen
    INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2023, 239
  • [25] Design theory and dynamic analysis of a deployable boom
    Chu, ZhongYi
    Lei, YiAn
    MECHANISM AND MACHINE THEORY, 2014, 71 : 126 - 141
  • [26] Scissor-hinged deployable structures for inclined roofs
    Freire-Tellado, M. J.
    Munoz-Vidal, M.
    Lopez-Cesar, I
    Perez-Valcarcel, J.
    INFORMES DE LA CONSTRUCCION, 2019, 71 (556) : 1 - 12
  • [27] Dynamic Analysis and Simulation of Deployable Planar Truss Mechanism
    Sun, Y.
    Shi, G. K.
    Shan, J. H.
    Dong, M. F.
    ULTRA-PRECISION MACHINING TECHNOLOGIES, 2009, 69-70 : 649 - 654
  • [28] Dynamic modeling and simulation for the flexible spacecraft with dynamic stiffening
    李崔春
    孟秀云
    刘藻珍
    JournalofBeijingInstituteofTechnology, 2015, 24 (03) : 305 - 312
  • [29] A Deployable Conical Log Spiral Antenna for Small Spacecraft: Electronic Design and Test
    Williams, Lewis R.
    Hoel, Karina Vieira
    Braten, Lars Erling
    Romeijer, Arthur
    Hjermann, Natanael
    Sagsveen, Bendik
    AEROSPACE, 2025, 12 (03)
  • [30] Calculation of spacecraft deployable elements dynamics
    Garifullin, MF
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 2000, (04): : 3 - 6
12345