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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 |
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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.
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Received: 13 July 2020
Published: 21 June 2021
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