Authors' response to the rebuttal by A. Cushman

Q. Hu; B. Xiao

doi:10.1007/s11071-011-0008-4

Authors' response to the rebuttal by A. Cushman

Q. Hu
, B. Xiao

Harbin Institute of Technology

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
卷	64
期	4
DOI	https://doi.org/10.1007/s11071-011-0008-4
出版状态	已出版 - 6月 2011
已对外发布	是

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title = "Authors' response to the rebuttal by A. Cushman",

abstract = "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).",

keywords = "Adaptive control, Fault tolerant control, Flexible spacecraft",

author = "Q. Hu and B. Xiao",

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AU - Xiao, B.

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AB - 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).

KW - Adaptive control

KW - Fault tolerant control

KW - Flexible spacecraft

UR - https://www.scopus.com/pages/publications/79959502079

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DO - 10.1007/s11071-011-0008-4

M3 - 文献综述

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SN - 0924-090X

VL - 64

SP - 413

EP - 414

JO - Nonlinear Dynamics

JF - Nonlinear Dynamics

IS - 4

ER -

Authors' response to the rebuttal by A. Cushman

摘要

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