Volume 13 Issue 2
Apr.  2020
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LI Hua-dong, QI Ke-qi, SHI Qiang, WANG Shao-xin, WANG Zhi. Performance test of piezoelectric actuators for space inertial sensors[J]. Chinese Optics, 2020, 13(2): 344-353. doi: 10.3788/CO.20201302.0344
Citation: LI Hua-dong, QI Ke-qi, SHI Qiang, WANG Shao-xin, WANG Zhi. Performance test of piezoelectric actuators for space inertial sensors[J]. Chinese Optics, 2020, 13(2): 344-353. doi: 10.3788/CO.20201302.0344

Performance test of piezoelectric actuators for space inertial sensors

doi: 10.3788/CO.20201302.0344
Funds:

Leading Special Project of Chinese Academy of Sciences XDA15020704

More Information
  • Corresponding author: WANG Zhi, E-mail:wz070611@126.com
  • Received Date: 03 Nov 2019
  • Rev Recd Date: 09 Dec 2019
  • Publish Date: 01 Apr 2020
  • In order to ensure the normal operation of space inertial sensors in orbit, it is necessary to ensure the test mass is fixed during launch to prevent collision with the surrounding capacitor plate. It must grab the test mass after reaching its predetermined orbit and precisely release it in its correct position with minimal residual velocity such that it remains free-floating. In this paper, a piezoelectric linear actuator that is used to grab the test mass is designed, customized and tested for performance. The test results show that the customized piezoelectric actuator can achieve a minimum step size of less than 1 nm, but the step length stability error is large; the maximum driving force at 150 V of input is 72 N; the single stepping drive force is stable; during the process of fixing the test mass, the driving force is stable and the deviation in its stability is 0.16%. These findings meet the needs of the grabbing, positioning, and release mechanisms.

     

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