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

Research output: Contribution to journal › Review article › peer-review

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).

Original language	English
Pages (from-to)	413-414
Number of pages	2
Journal	Nonlinear Dynamics
Volume	64
Issue number	4
DOIs	https://doi.org/10.1007/s11071-011-0008-4
State	Published - Jun 2011
Externally published	Yes

Keywords

Adaptive control
Fault tolerant control
Flexible spacecraft

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10.1007/s11071-011-0008-4

Cite this

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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",

year = "2011",

month = jun,

doi = "10.1007/s11071-011-0008-4",

language = "英语",

volume = "64",

pages = "413--414",

journal = "Nonlinear Dynamics",

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publisher = "Springer Netherlands",

number = "4",

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T1 - Authors' response to the rebuttal by A. Cushman

AU - Hu, Q.

AU - Xiao, B.

PY - 2011/6

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N2 - 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).

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

U2 - 10.1007/s11071-011-0008-4

DO - 10.1007/s11071-011-0008-4

M3 - 文献综述

AN - SCOPUS:79959502079

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

Abstract

Keywords

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