Quadrotor Fault Tolerant Incremental Sliding Mode Control driven by Sliding Mode Disturbance Observers

被引:76
|
作者
Wang, Xuerui [1 ]
Sun, Sihao [1 ]
van Kampen, Erik-Jan [1 ]
Chu, Qiping [1 ]
机构
[1] Delft Univ Technol, Kluyverweg 1, NL-2629 HS Delft, Netherlands
关键词
Incremental Nonlinear Dynamic Inversion; Fault-Tolerant Control; Sliding Mode Disturbance Observer; Sliding Mode Control; Quadrotor flight tests; NONLINEAR DYNAMIC INVERSION; TRAJECTORY TRACKING CONTROL; ATTITUDE-CONTROL; VEHICLE CONTROL; UAV;
D O I
10.1016/j.ast.2019.03.001
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper proposes an Incremental Sliding Mode Control driven by Sliding Mode Disturbance Observers (INDI-SMC/SMDO), with application to a quadrotor fault tolerant control problem. By designing the SMC/SMDO based on the control structure of the sensor-based Incremental Nonlinear Dynamic Inversion (INDI), instead of the model-based Nonlinear Dynamic Inversion (NDI) in the literature, the model dependency of the controller and the uncertainties in the closed-loop system are simultaneously reduced. This allows INDI-SMC/SMDO to passively resist a wider variety of faults and external disturbances using continuous control inputs with lower control and observer gains. When applied to a quadrotor, both numerical simulations and real-world flight tests demonstrate that INDI based SMC/SMDO has better performance and robustness over NDI based SMC/SMDO, in the presence of model uncertainties, wind disturbances, and sudden actuator faults. Moreover, the implementation process is simplified because of the reduced model dependency and smaller uncertainty variations of INDI-SMC/SMDO. Therefore, the proposed control method can be easily implemented to improve the performance and survivability of quadrotors in real life. (C) 2019 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:417 / 430
页数:14
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