Fully actuated system approach to attitude control of flexible spacecraft with nonlinear time-varying inertia
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Computer Science
Link
https://link.springer.com/content/pdf/10.1007/s11432-021-3349-3.pdf
Reference34 articles.
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3. Meng B, Zhao Y. The dynamics characteristics of flexible spacecraft and its closed-loop stability with passive control. J Syst Sci Complex, 2021, 34: 860–872
4. Xiao B, Hu Q L, Zhang Y M. Fault-tolerant attitude control for flexible spacecraft without angular velocity magnitude measurement. J Guid Control Dyn, 2011, 34: 1556–1561
5. Zhang R, Qiao J Z, Li T, et al. Robust fault-tolerant control for flexible spacecraft against partial actuator failures. Nonlinear Dyn, 2014, 76: 1753–1760
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