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Analysis and Control of Flexible Multibody Deployment

  • Baoyan Duan
  • Yiqun Zhang
  • Jingli Du
Chapter
  • 17 Downloads
Part of the Springer Tracts in Mechanical Engineering book series (STME)

Abstract

The law of universal gravitation, proposed by Newton, provides the theoretical basis for the development of artificial satellites, which consist of the proprietary system and support system. The deployable antenna is an important part of the proprietary system.

References

  1. 1.
    Li TJ (2012) Deployment analysis and control of deployable antenna. Aerosp Sci Technol 18(1):42–47CrossRefGoogle Scholar
  2. 2.
    Kashni K (1988) Representation of cables in space subjected to uniformly distributed loads. Int J Space Struct 3(4):221–230CrossRefGoogle Scholar
  3. 3.
    Zhang YQ, Yang DW, Li SL (2016) An integrated control and structural design approach for mesh reflector deployable space antennas. Mechatronics 35:71–81CrossRefGoogle Scholar

Copyright information

© Springer Nature Singapore Pte Ltd. 2020

Authors and Affiliations

  • Baoyan Duan
    • 1
  • Yiqun Zhang
    • 2
  • Jingli Du
    • 3
  1. 1.School of Electro-Mechanical EngineeringXidian UniversityXi’anChina
  2. 2.School of Electro-Mechanical EngineeringXidian UniversityXi’anChina
  3. 3.School of Electro-Mechanical EngineeringXidian UniversityXi’anChina

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