The stochastic sliding mode variable structure guidance laws based on optimal control theory
作者： Hongqiang Wang , Daiqiang Cao , Xudong Wang
DOI: 10.1007/S11768-013-1031-4
关键词:
摘要: A stochastic sliding-mode variable structure guidance law involving optimal control theory is presented for the missile target intercept model, in which state noise, uncertain system parameters, movement and measured noise are considered. This synthesizes merits of with line-of-sight rate convergence strong robustness. Through theoretic analysis, it proved that sliding mode hyperplane sub-achievable closed loop system. The numerical results show effectiveness proposed algorithm.
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