Volume 43 Issue 1
Jan.  2013
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YUE Baozeng, SONG Xiaojuan. ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT[J]. Advances in Mechanics, 2013, 43(1): 163-173. doi: 10.6052/1000-0992-12-025
Citation: YUE Baozeng, SONG Xiaojuan. ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT[J]. Advances in Mechanics, 2013, 43(1): 163-173. doi: 10.6052/1000-0992-12-025

ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT

doi: 10.6052/1000-0992-12-025
Funds:  The project was supported by the Natural Science Foundation of China(10772026,11072030),Ph.D.Programs Foundation of Ministry of Education of China(20080010011).
More Information
  • Corresponding author: YUE Baozeng
  • Received Date: 2012-03-01
  • Rev Recd Date: 2012-07-09
  • Publish Date: 2013-01-24
  • This paper summarized the recent research progress about the attitude nonlinear dynamics of liquid filled spacecraft and coupling dynamics of multi-body-liquid-control nonlinear systems. The developments and achievements in some important research fields, such as dynamics modeling of liquidlled spacecraft with flexible appendage, liquid sloshing dynamics modeling, nonlinear theory and method for spacecrafts with coupling of multi-body-liquid-control, numerical simulation and experiments, are reviewed. The prospects of future researches on concerned topics are also presented in the final section.

     

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