强化学习
航空学
计算机科学
控制(管理)
钢筋
航空航天工程
汽车工程
工程类
控制工程
人工智能
结构工程
作者
Mo Zhai,Zhiqi Zhang,Shuaichen Nie,Shouzhao Sheng
标识
DOI:10.1109/csat61646.2023.00136
摘要
In view of the problem of auto-disturbance rejection flight control of compound coaxial high speed helicopter, the maneuvering methods in different flight stages are analyzed first. Then, based on ADRC control theory, using the idea of cascade control, the controller design is analyzed for inner loop attitude control and outer loop speed/position control. Besides, the ADRC parameters are adjusted by DQN algorithm. Finally, MATLAB mathematical simulation is carried out to verify and analyze the feasibility and effectiveness of the proposed scheme.
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