Attitude control of short-range loitering missile based on ADRC

ADRC (ADRC) has excellent control performance. The paper Introduces structure and discrete algorithms of the ADRC,and describes its parameter tuning rule. The ADRC control technology is applied to attitude control system design of short-range loitering missile, from the perspective of engineering applications, proposesing a design method of ADRC attitude controller, specifically addressing the principle of the method and process. Simulation results show that this method has strong robustness and adaptability, strong dynamic performance and stable performance.