终端滑动模式
控制理论(社会学)
弹道
计算机科学
控制器(灌溉)
参数统计
滑模控制
趋同(经济学)
Lyapunov稳定性
MATLAB语言
自适应控制
控制工程
工程类
控制(管理)
数学
人工智能
物理
统计
生物
非线性系统
农学
经济
操作系统
量子力学
天文
经济增长
作者
Nasim Ullah,Yasir Mehmood,Jawad Aslam,Amjad Ali,Jamshed Iqbal
出处
期刊:IEEE Access
[Institute of Electrical and Electronics Engineers]
日期:2021-01-01
卷期号:9: 74385-74405
被引量:31
标识
DOI:10.1109/access.2021.3081483
摘要
Leader follower formation of unmanned aerial vehicles (UAVs) and unmanned ground vehicles (UGVs) has found numerous applications such as surveillance of critical infrastructure, industrial automation and disaster management emergency. For completion of high precision group tasks, the choice of appropriate control mechanism is of utmost importance. In presence of environmental effects,external disturbances and parametric uncertainties in the UAVs and UGV models, the controller design process is a challenging task. In order to address the aforementioned problems and to ensure minimum tracking errors and fast convergence of the states, this article proposes an adaptive robust formation and trajectory tracking control scheme for a leader follower formation of UAVs and UGV using Non-Singular Terminal Super Twisting Sliding Mode Control Method.Adaptive compensators are derived based on Lyapunov function method and stability of the proposed controllers is guaranteed. Two variants of the control schemes namely Adaptive Super Twisting SMC (AST-SMC) and Adaptive Non-Singular Terminal Super Twisting SMC (ANSTS-SMC) are tested using numerical simulations performed in MATLAB/Simulink. From the results presented, and with the proposed ANSTS-SMC control scheme, the measured [X Y] tracking errors for leader, follower1 and follower2 UAVs are [0 0.01]m, [0.01 0.02]m and [0.01, 0.02]m respectively, While with the AST-SMC method the peak [X Y] tracking errors for leader, follower1 and follower2 UAVs are [0.05 0.05]m, [0.1 0.2]m and [0.05 0.1]m respectively. The proposed leader follower formation can be effectively used to monitor solar/PV panels and cables in large solar parks.
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