Abstract detail

54 / 2021-03-28 23:14:34
Micro-Vibration Control in High Precision Spacecraft
High Precision Spacecraft;Micro-Vibration;Measurement and Control;Test Verification
Noise and vibration control
Abstract Accepted
Yaoqi FENG / Beijing Institute of Spacecraft Environment Engineering
This paper presents at first the research background of micro-vibration problem for high precision spacecraft; the key micro-vibration techniques involved during the development process of high precision spacecraft are introduced, which are concerning micro-vibration measurement and analysis, micro-vibration control, micro-vibration test verification. Then, the paper gives the features and challenges of micro-vibration measurement and analysis; the difficult points, the technical ways, and the engineering applications of micro-vibration control for high precision spacecraft are described, which are concerning essentially the integrated analysis-design approach for micro-vibration control, and the development technique for micro-vibration isolators; the micro-vibration test techniques for disturbance equipment, sensitive payload, and for the whole spacecraft are presented in details. Finally, the paper summarizes briefly the technical development status of micro-vibration control for high precision spacecraft, and an outlook for the future development of micro-vibration techniques is also given.

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Important Dates

Abstract Submission Deadline:

 31st March 2021 15th April 2021

Extended Deadline: 1st Aug. 2022

 

Abstract Acceptance:

30th April  2021 Rollover

 

Full Paper Submission Deadline:

30th June 2021  14th July 2021

Extended Deadline: 15th Aug. 2022 

 

Notification of Acceptance:

15th August 2021 1st Sept. 2021

1st Sept. 2022

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