TY - JOUR
T1 - 基于参数估计的四旋翼无人机自适应鲁棒路径跟随控制器
AU - Xiu, Yang
AU - Deng, Hongbin
AU - Wei, Yiran
AU - Li, Dongfang
N1 - Publisher Copyright:
© 2022 China Ordnance Society. All rights reserved.
PY - 2022/8
Y1 - 2022/8
N2 - To improve the path following accuracy and flight robustness of quadrotor UAVs, an adaptive robust path following controller based on parameter estimation is proposed. The controller can adaptively estimate the gyroscopic factors and drag coefficients for the UAV model, compensate the system’s control input based on estimated values, and offset the negative impact of the external environment with an anti-interference capacity. The controller can effectively improve the path following and anti-interference performance of quadrotor UAVs. First, a nonlinear mechanical model of a quadrotor UAV is established. Second, the path following targets for UAVs are divided into attitude angle targets and moving position targets. Third, the backstepping sliding mode method and adaptive control method are used to design the control input equation and the estimation updating law of the UAV. Simultaneously, the asymptotic stability of the UAV attitude system and motion position system is verified by applying the Lyapunov method. Lastly, the effectiveness and superiority of the proposed controller are verified by simulation and experiments.
AB - To improve the path following accuracy and flight robustness of quadrotor UAVs, an adaptive robust path following controller based on parameter estimation is proposed. The controller can adaptively estimate the gyroscopic factors and drag coefficients for the UAV model, compensate the system’s control input based on estimated values, and offset the negative impact of the external environment with an anti-interference capacity. The controller can effectively improve the path following and anti-interference performance of quadrotor UAVs. First, a nonlinear mechanical model of a quadrotor UAV is established. Second, the path following targets for UAVs are divided into attitude angle targets and moving position targets. Third, the backstepping sliding mode method and adaptive control method are used to design the control input equation and the estimation updating law of the UAV. Simultaneously, the asymptotic stability of the UAV attitude system and motion position system is verified by applying the Lyapunov method. Lastly, the effectiveness and superiority of the proposed controller are verified by simulation and experiments.
KW - adaptive robust
KW - backstepping sliding mode
KW - path following
KW - quadrotor UAV
UR - http://www.scopus.com/inward/record.url?scp=85137769715&partnerID=8YFLogxK
U2 - 10.12382/bgxb.2021.0444
DO - 10.12382/bgxb.2021.0444
M3 - 文章
AN - SCOPUS:85137769715
SN - 1000-1093
VL - 43
SP - 1926
EP - 1938
JO - Binggong Xuebao/Acta Armamentarii
JF - Binggong Xuebao/Acta Armamentarii
IS - 8
ER -