Circularly Constrained Particle Motion in Spinning and Coning Bodies
Author:
Affiliation:
1. University of California, Los Angeles, Calif.
2. Hughes Aircraft Company, El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49544
Reference8 articles.
1. Nutation damping and vibration isolation in a flexibly coupled dual-spin spacecraft
2. Dynamically unbalanced dual-spin space stations with rigid or low-coupling interconnections
3. An Automatic Mass-Trim System for Spinning Spacecraft
4. Harrison, J. A. "A Device for Automatically Balancing a Spinning Spacecraft," Ph.D. thesis,July 1972, University of California, Los Angeles, Calif.
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. References;The Method of Normal Forms;2011-08-16
2. Nutation Time Constant Determination of On-Axis Diaphragm Tanks on Spinner Spacecraft;Journal of Spacecraft and Rockets;2005-05
3. Bibliography;Applied Nonlinear Dynamics;1995-03-29
4. Nutation damping of spinning satellite with viscous annular dampers;Acta Astronautica;1989-12
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