Authors' response to the rebuttal by A. Cushman

Q. Hu, B. Xiao

Research output: Contribution to journalReview articlepeer-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 languageEnglish
Pages (from-to)413-414
Number of pages2
JournalNonlinear Dynamics
Volume64
Issue number4
DOIs
StatePublished - Jun 2011
Externally publishedYes

Keywords

  • Adaptive control
  • Fault tolerant control
  • Flexible spacecraft

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