Analysis and Optimization of Microvibration Isolation for Multiple Flywheel Systems of Spacecraft
Author:
Affiliation:
1. National University of Defense Technology, 410073 Changsha, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053885
Reference34 articles.
1. Modelling and testing of a soft suspension design for a reaction/momentum wheel assembly
2. Image Stabilization System for Hinode (Solar-B) Solar Optical Telescope
3. On-orbit jitter control in momentum actuators using a three-flywheel system
4. Analysis and Testing of Microvibrations Produced by Momentum Wheel Assemblies
5. DEVELOPMENT AND VALIDATION OF REACTION WHEEL DISTURBANCE MODELS: EMPIRICAL MODEL
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