Adaptive Sliding Mode & Nussbaum Gain Hybrid Control of Supersonic Missiles with Unknown Control Direction
نویسندگان
چکیده
A new nonlinear sliding mode, which can be expended and used in a large family nonlinear systems , is skillfully constructed for supersonic missile control with unknown control direction. Later, by using of the Nussbaum gain method, the unknown control direction problem is solved and also the appearance of control singularity was avoided. So the nonlinear sliding mode method and Nussbaum gain method are integrated perfectly in this paper and neither one is dispensable. Finally, this method is applided in supersonic missile system and the simulation result shows the rightness of the proposed method.
منابع مشابه
Adaptive Control of Supersonic Missiles with Unknown Input Coefficients
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