Compound Control System Design with Lateral Thrust and Aerodynamic Force Based on ADRC Method
LIU Kai, YANG Baoqing
School of Astronautics,Harbin Institute of Technology,Harbin 150001,Heilongjiang,China
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.
Key words :
aerodynamic and lateral thrust control
attitude control system
ADRC
ignition logic
simulation
Received: 13 July 2020
Published: 21 June 2021
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