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 language | English |
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Pages (from-to) | 2318-2323 |
Number of pages | 6 |
Journal | Optik |
Volume | 126 |
Issue number | 20 |
DOIs | |
Publication status | Published - 1 Oct 2015 |
Keywords
- Actuator fault
- Chattering-free
- Guidance law
- Impact angle
- Sliding mode control