Experimental Study on Integrated Servo Control for Canard-Controlled Missiles

Abstract

This paper describes an experimental study on an integrated servo control method. Conventional servo control schemes may experience performance degradation under the presence of physical constraints. An integrated scheme is proposed in this study to address this problem. In the proposed method, three controllers correspond to autopilot commands directly instead of four actuators. Various simulations and experiments show that the proposed integrated servo control method provides better performance than the conventional ones