Abstract：Compound control scheme with aerodynamic force and lateral thrust is proposed based on the established short-period, linearized motion model of compound-control missile. The aerodynamic control subsystem uses three-loop control structure. Overload loop adopts PI control. The angle of attack loop and the angular velocity loop adopt active disturbance rejection control (ADRC). Then aerodynamic/lateral thrust distribution strategy is designed according to the fuzzy control and the ignition logic of the lateral thrust control subsystem is designed with the vector synthesis method. Finally, a specific simulation scenario is designed and verified in Matlab. The results show that a small miss distance can also be ensured during the interception of high-altitude targets. The composite control scheme ensures that the system has rapid overload response characteristics and good stability, which proves that the algorithm in the paper is effective.
刘凯, 杨宝庆. 一种基于自抗扰方法的姿控直气复合控制系统设计[J]. 空天防御, 2021, 4(2): 40-47.
LIU Kai, YANG Baoqing. Compound Control System Design with Lateral Thrust and Aerodynamic Force Based on ADRC Method. Air & Space Defense, 2021, 4(2): 40-47.
