Adaptive Robust Trajectory Tracking Control of Multiple Quad-Rotor UAVs with Parametric Uncertainties and Disturbances

被引:25
作者
Mehmood, Yasir [1 ]
Aslam, Jawad [1 ]
Ullah, Nasim [2 ]
Chowdhury, Md. Shahariar [3 ]
Techato, Kuaanan [3 ,4 ]
Alzaed, Ali Nasser [5 ]
机构
[1] Natl Univ Sci & Technol, Sch Mech & Mfg Engn, Islamabad 44000, Pakistan
[2] Taif Univ, Coll Engn, Dept Elect Engn, POB 888, Al Hawiyah, Taif, Saudi Arabia
[3] Prince Songkla Univ, Fac Environm Management, Hat Yai 90112, Thailand
[4] Prince Songkla Univ, Fac Environm Management, Environm Assessment & Technol Hazardous Waste Man, Hat Yai 90112, Thailand
[5] Taif Univ, Coll Engn, Dept Architecture Engn, POB 888, Al Hawiyah, Taif, Saudi Arabia
关键词
quad-rotor control; adaptive robust control; super twisting sliding mode control; formation control; SLIDING-MODE CONTROL; FOLLOWER FORMATION CONTROL; UNMANNED AERIAL VEHICLES; QUADROTOR; DESIGN; FEEDBACK;
D O I
10.3390/s21072401
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
Recently, formation flying of multiple unmanned aerial vehicles (UAVs) found numerous applications in various areas such as surveillance, industrial automation and disaster management. The accuracy and reliability for performing group tasks by multiple UAVs is highly dependent on the applied control strategy. The formation and trajectories of multiple UAVs are governed by two separate controllers, namely formation and trajectory tracking controllers respectively. In presence of environmental effects, disturbances due to wind and parametric uncertainties, the controller design process is a challenging task. This article proposes a robust adaptive formation and trajectory tacking control of multiple quad-rotor UAVs using super twisting sliding mode control method. In the proposed design, Lyapunov function-based adaptive disturbance estimators are used to compensate for the effects of external disturbances and parametric uncertainties. The stability of the proposed controllers is guaranteed using Lyapunov theorems. Two variants of the control schemes, namely fixed gain super twisting SMC (STSMC) and adaptive super twisting SMC (ASTSMC) are tested using numerical simulations performed in MATLAB/Simulink. From the results presented, it is verified that in presence of disturbances, the proposed ASTSMC controller exhibits enhanced robustness as compared to the fixed gain STSMC.
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页数:24
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