The Dynamics Characteristics of Flexible Spacecraft and its Closed-Loop Stability with Passive Control
Author:
Publisher
Springer Science and Business Media LLC
Subject
Information Systems,Computer Science (miscellaneous)
Link
http://link.springer.com/content/pdf/10.1007/s11424-020-9268-8.pdf
Reference11 articles.
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2. Malekzadeh M, Naghash A, and Talebi H A, Robust attitude and vibration control of nonlinear flexible spacecraft, Asian Journal of Control, 2012, 14(2): 553–563.
3. Nakka Y K, Chung S, Allison J T, et al., Nonlinear attitude control of a spacecraft with distributed actuation of solar arrays, Journal of Guidance, Control, and Dynamics, 2019, 42(3): 458–475.
4. Wang Z H, Jia Y H, Xu S J, et al., Active vibration suppression in flexible spacecraft with optical measurement, Aerospace Science and Technology, 2016, 55: 49–56.
5. Yu Y N, Meng X Y, Li K H, et al., Robust control of flexible spacecraft during large-angle attitude maneuver, Journal of Guidance, Control, and Dynamics, 2014, 37(3): 1027–1033.
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