Sliding mode based impact angle guidance law considering actuator fault

Shaoming He*, Defu Lin

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

8 Citations (Scopus)

Abstract

In this paper, a new continuous impact angle constraint guidance law in the presence of actuator fault is presented based on sliding mode control theory. The robustness and finite-time convergence of the basic guidance law is established using Lyapunov stability theory. For actuator compensation, an additional term is augmented in the original guidance law to guarantee finite-time stability of the closed-loop guidance system. Theoretical analysis and simulation results demonstrate the effectiveness of the proposed method.

Original languageEnglish
Pages (from-to)2318-2323
Number of pages6
JournalOptik
Volume126
Issue number20
DOIs
Publication statusPublished - 1 Oct 2015

Keywords

  • Actuator fault
  • Chattering-free
  • Guidance law
  • Impact angle
  • Sliding mode control

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