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Plasma aerodynamic excitation based on surface dielectric discharge is a effective approach for flow control, which can significantly improve the aerodynamic characteristics of the aircraft. However, the plasma excitation interaction region is limited and there are no significant effects by using typical two-electrodes sustained by nanosecond-pulse dielectric barrier discharge, therefore, it is difficult...
Nonlinear inverse dynamic controller based on differential flatness was designed for Glide-reentry anti-vessel missile terminal engineless part. Aerodynamic data was processed to make the missile model flat. Brake rudder was introduced to control terminal energy and fulfill the requirement of flatness.
In this paper, a novel algorithm model-following adaptive second-order sliding model control is proposed for nonlinear uncertain systems. Second-order sliding model control can effectively overcome chattering that conventional sliding model control hold. The difference between the output of pant and the output of the followed model is regarded as sliding variable; the algorithm presented here introduced...
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