| Citation: | ZHANG J，WEN C，YANG X，et al. Design of an electric drive aircraft tug control system based on ADRC[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（5）：1017-1026 （in Chinese） doi: 10.13700/j.bh.1001-5965.2021.0377
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Large inertia, a high center of mass, and time-varying friction are aspects of the aircraft towing process that have a significant impact on the stability of the aircraft tug. In order to improve the stability of the electric aircraft tug, the variable speed and torque that affect the stability of aircraft traction are taken as the research objects, and the control effect of the designed strategy is analyzed. Using ADAMS and MATLAB/Simulink simulation software, the aircraft and tug dynamic model and motor model are constructed, and the second-order nonlinear auto disturbance rejection controller based on speed and torque is designed. The dynamic characteristics of the wheel speed of the aircraft tug based on active disturbance rejection control (ADRC) and PID control during the shifting process are compared and analyzed, and the prototype control test of the shifting process is carried out. The results show that the aircraft traction system based on the second-order nonlinear auto-disturbance rejection control algorithm has better gear shifting effects, and the wheel speed during gear shifting is better in terms of response speed, stability and anti-disturbance ability; the test results match the simulation results, and the coincidence proves the feasibility and correctness of the simulation model and simulation results, which lays the foundation for the research of highly stable aircraft tug.
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