Authors' response to the rebuttal by A. Cushman

Q. Hu, B. Xiao

科研成果: 期刊稿件文献综述同行评审

摘要

This is a response to the rebuttal by A. Cushman regarding our paper "Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness" (Nonlinear Dyn. doi: 10.1007/s11071-011- 0007-5, 2011).

源语言英语
页(从-至)413-414
页数2
期刊Nonlinear Dynamics
64
4
DOI
出版状态已出版 - 6月 2011
已对外发布

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