Parametric Studies of the Whole Spacecraft Vibration Isolation
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics, 100083 Beijing, People’ s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.7306
Reference12 articles.
1. Multi-axis whole-spacecraft vibration isolation for small launch vehicles
2. Vibration Isolation Review: II. Shock Excitation
3. Vibration Isolation of Launch Vehicle Payload and Its Subsystem
4. Decentralized control for multichannel active vibration isolation
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