Volume 18 Issue 1
Jan.  1998
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YU Dengyun, QU Guangji, ZENG Xin, WANG Ning. CONTACT-IMPACT DYNAMIC ANALYSIS OF SPACECRAFT IN THE COURSE OF SPACE DOCKING[J]. Chinese Journal of Space Science, 1998, 18(1): 62-68. doi: 10.11728/cjss1998.01.062
Citation: YU Dengyun, QU Guangji, ZENG Xin, WANG Ning. CONTACT-IMPACT DYNAMIC ANALYSIS OF SPACECRAFT IN THE COURSE OF SPACE DOCKING[J]. Chinese Journal of Space Science, 1998, 18(1): 62-68. doi: 10.11728/cjss1998.01.062

CONTACT-IMPACT DYNAMIC ANALYSIS OF SPACECRAFT IN THE COURSE OF SPACE DOCKING

doi: 10.11728/cjss1998.01.062 cstr: 32142.14.cjss1998.01.062
  • Received Date: 1997-01-06
  • Rev Recd Date: 1997-09-26
  • Publish Date: 1998-01-24
  • The contact-impact dynamics in the course of spacecraft docking is the basis of research and design of docking mechanism of manned-space vehicle. According to the docking mechanism of androgynous and peripheral type, a contact-impact dynamic model and an explicit expression of impact load are given in this paper by using the vector mechanics and visco-elasticity. The targeting calculation and statistical analysis of an engineering sample is used to illustrate the method, and a satisfying result is obtained.

     

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