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Research on Design and Analysis Platform for Modular Spacecraft

In: The 19th International Conference on Industrial Engineering and Engineering Management

Author

Listed:
  • Xiao-wen Zeng

    (Hunan Institute of Science and Technology)

  • Zhao-xia He

    (Chang’an University)

  • Hao Luo

    (Northwestern Polytechnical University)

Abstract

In spacecraft structure design process, modular technology is very important for improving efficiency and reducing cost. Based on the modular design method, a deployable on-orbit spacecraft modular configuration was established. The influence of simultaneously deployment solar panel and modular structures under the situation of weightlessness on the spacecraft’s gesture was simulated and analyzed with the assistance of virtual prototype technology. The simulated result shows that the deployment of module structures is vital to the angle of spacecraft’s gesture and its velocity. Within the Eclipse development environment, an integrated platform which includes design and analysis for spacecraft was developed with J2EE. In order to acquire rapid response to the whole process, which includes structural design, digital prototype assembly and dynamics analysis, the structure design, assembly and dynamics analysis of spacecraft were well integrated.

Suggested Citation

  • Xiao-wen Zeng & Zhao-xia He & Hao Luo, 2013. "Research on Design and Analysis Platform for Modular Spacecraft," Springer Books, in: Ershi Qi & Jiang Shen & Runliang Dou (ed.), The 19th International Conference on Industrial Engineering and Engineering Management, edition 127, chapter 0, pages 1263-1272, Springer.
    • Handle: RePEc:spr:sprchp:978-3-642-38391-5_133
    DOI: 10.1007/978-3-642-38391-5_133
    as

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