Synthesis of Nonlinear Model Matching Control System and Its Application to Flight System
نویسندگان
چکیده
The proposed control method is based on Hirschorn's Algorithm extended with Silverman's structure algorithm, and facilitates easy determination of the control law using the relationship, between the output and the input, which is obtained by differentiating the output. This method is the extension of the linear model matching control system for which the control law was proposed by Wolovich. The proposed control system is applied to a flight control system (for example, pitch angle, vertical velocity and C* control system) and numerical simulations are shown to investigate the feasibility of the proposed approach.
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تاریخ انتشار 2014