Adaptive sliding mode robust control based on multi-dimensional Taylor network for trajectory tracking of quadrotor UAV

被引:13
作者
Wang, Guo-Biao [1 ,2 ]
机构
[1] Southeast Univ, Sch Automat, Nanjing 210096, Peoples R China
[2] Minist Educ, Key Lab Measurement & Control Complex Syst Engn, Nanjing 210096, Peoples R China
关键词
autonomous aerial vehicles; uncertain systems; Lyapunov methods; robust control; nonlinear control systems; adaptive control; attitude control; stability; position control; control system synthesis; velocity control; variable structure systems; linear state transformation; unknown external disturbances; original kinetic model; control design; mode technique; neural networks; MTN; position tracking error; attitude tracking error; fuselage load identification error; trajectory tracking control scheme; multidimensional Taylor network; mode robust control theory; adaptation laws; quadrotor unmanned aerial vehicle; composite disturbance; external multiple interference; H-INFINITY CONTROL; NONLINEAR-SYSTEMS; CONTROL DESIGN; PATH TRACKING;
D O I
10.1049/iet-cta.2019.1058
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this study, multi-dimensional Taylor network (MTN) inspired sliding mode robust control theory based adaptation laws are proposed to realise trajectory tracking for a quadrotor unmanned aerial vehicle. Compared with existing methods, the composite disturbance considered in this study includes external multiple interference and fuselage parameter perturbation, which is more in accord with reality. Through a linear state transformation, the uncertain coefficients and unknown external disturbances are grouped together and the original kinetic model is decoupled into two subsystems of position and attitude that make the control design become feasible. MTNs are used to compensate the lumped non-linearities, and the adaptive sliding mode technique is employed to construct the controller. Different from the controllers based on neural networks, MTN contains only addition and multiplication, which greatly lessens the computational complexity and improves the real-time performance. By the Lyapunov theory, the position tracking error, attitude tracking error and fuselage load identification error are bounded in probability have been proved and the stability of the system is guaranteed. Simulation studies demonstrate the effectiveness and superiority of the proposed trajectory tracking control scheme.
引用
收藏
页码:1855 / 1866
页数:12
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