Research Progress on Distributed Active Vibration Absorber to Spacecraft in Inner Sound Field Control
Received:April 19, 2019  Revised:May 05, 2019
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DOI:10.7643/issn.1672-9242.2019.12.007
KeyWord:distributed active vibration absorber  sound field active control  spacecraft  DAVA
                 
AuthorInstitution
YUAN Kai Science and Technology on Reliability and Environment Engineering Laboratory, Beijing Institute of Structure and Environment Engineering, Beijing , China
ZHANG Zhong Science and Technology on Reliability and Environment Engineering Laboratory, Beijing Institute of Structure and Environment Engineering, Beijing , China
GAO Bo Science and Technology on Reliability and Environment Engineering Laboratory, Beijing Institute of Structure and Environment Engineering, Beijing , China
QIN Zhao-hong Science and Technology on Reliability and Environment Engineering Laboratory, Beijing Institute of Structure and Environment Engineering, Beijing , China
REN Fang Science and Technology on Reliability and Environment Engineering Laboratory, Beijing Institute of Structure and Environment Engineering, Beijing , China
HOU Chuan-tao Science and Technology on Reliability and Environment Engineering Laboratory, Beijing Institute of Structure and Environment Engineering, Beijing , China
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Abstract:
      In terms of inner sound field control to spacecraft, the research progress of DAVA in spacecraft was discussed in device improving, sound field control method and application. Some problems like multiphysics coupling modeling method, controller design method under complex noise environment and power consumption in research and development of DAVA intelligent device for inner sound field control to spacecraft were summarized. Research on sound field control of launch vehicle fairing was performed. The future application of DAVA in launch vehicle fairing was expected.
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