Rebuttal to "Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness" Response

被引：0
|
作者：
Hu, Q. [1 ]
Xiao, B. [1 ]
机构：
[1] Harbin Inst Technol, Dept Control Sci & Engn, Harbin 150001, Peoples R China
来源：
NONLINEAR DYNAMICS | 2011年 / 64卷 / 04期
关键词：
Flexible spacecraft; Fault tolerant control; Adaptive control;
D O I：
10.1007/s11071-011-0008-4
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
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).
引用
收藏
页码：413 / 414
页数：2
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