Optimum Method for Microvibration Isolation of Spacecraft Reaction Wheel with Variable Rotating Speed
Author:
Affiliation:
1. National University of Defense Technology, 410073 Changsha, People’s Republic of China
2. Key Laboratory of Spacecraft In-Orbit Fault Diagnosis and Maintenance, 710043 Xi’an, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J063718
Reference46 articles.
1. DennehyC.Alvarez-SalazarO. S. “Spacecraft Micro-Vibration: A Survey of Problems, Experiences, Potential Solutions, and Some Lessons Learned,” NASA TM-2018-220075, 2018.
2. Experimental investigation of microvibrations induced by reaction wheels on earth observation satellite
3. Micro-vibration suppression methods and key technologies for high-precision space optical instruments
4. Advances in fine line-of-sight control for large space flexible structures
5. Improvement of micro-vibration of a two-stage Stirling cryocooler
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