High-order sliding mode observer-based trajectory tracking control for a quadrotor UAV with uncertain dynamics

被引:74
作者
Zhao, Zhenhua [1 ]
Cao, Dong [1 ]
Yang, Jun [2 ,3 ]
Wang, Huiming [4 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Peoples R China
[2] Southeast Univ, Sch Automat, Nanjing 210096, Peoples R China
[3] Shenzhen Res Inst, Southeast Univ, Shenzhen 518063, Peoples R China
[4] Chongqing Univ Posts & Telecommun, Chongqing Key Lab Complex Syst & Bion Control, Chongqing 400065, Peoples R China
关键词
Quadrotor UAV; Sliding mode observer; Nonsingular terminal sliding mode; Disturbance observer-based control (DOBC); Trajectory tracking; MISSILE;
D O I
10.1007/s11071-020-06050-2
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper investigates the trajectory tracking problem of the quadrotor unmanned aerial vehicles (UAV) with consideration of both attitude and position dynamics. First of all, the trajectory tracking problem is divided into the commands tracking in position and attitude loops by introducing the virtual attitude angle commands. Secondly, the high-order sliding mode observers (HSMOs) are introduced to estimate the lumped disturbances in position loop and the derivatives of the attitude angle tracking errors, the lumped disturbances in the attitude loop. And then the composite nonlinear dynamical inversion controller in position loop and the composite nonsingular terminal sliding mode controller in attitude loop are constructed by introducing the estimation information of HSMOs into controller design process. Finally, the simulations based on the data of a practical UAV are carried out to verify the effectiveness of the proposed method.
引用
收藏
页码:2583 / 2596
页数:14
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