摘要
四旋翼飞行控制系统是多输入强耦合的典型代表,为了探究自抗扰飞控算法的控制效果,文章对一款四旋翼进行动力学建模,将其控制模式简化为多通道模式,并利用Matlab中的Simulink搭建控制模型进行仿真。对其动态性能、抗干扰性和鲁棒性进行详细探讨,为四旋翼控制算法的实现与发展提供了结论支撑。
Four-rotator flight control system is a typical representative of multi-input strong coupling.In order to explore the control effect of the auto-disturbance rejection flight control algorithm,a four-rotator is modeled dynamically,its control mode is simplified to multi-channel mode,and the control model is built using Simulink in Matlab to simulate.The dynamic performance,anti-jamming and robustness of the four-rotator control algorithm are discussed in detail,which provides a conclusion support for the implementation and development of the four-rotator control algorithm.
作者
刘灵童
王旭
王大海
郑凯
尹晓娇
Liu Lingtong;Wang Xu;Wang Dahai;Zheng Kai;Yin Xiaojiao(School of Electronic Engineering,Xi’an Shiyou University,Xi’an 710065,China)
出处
《无线互联科技》
2022年第5期116-120,共5页
Wireless Internet Technology
基金
2020年陕西省大学生创新创业训练计划资助项目,项目编号:S202010705072。
