外部干扰下基于自适应神经网络的四旋翼无人机编队控制

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-09-20 DOI:10.1016/j.ast.2024.109608
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引用次数: 0

摘要

由多个四旋翼无人飞行器(UAV)组成的团队的编队控制可能会受到未知外部干扰的严重影响。外部干扰是由风力造成的空气动力干扰。本文探讨了多无人机系统在外部干扰影响下的鲁棒编队控制问题,使无人机之间保持稳定的网络连接,并维持分配给它们的不同编队。首先,开发了一个基于径向基函数神经网络(RBFNN)的模型,以对位置和姿态子系统的外部干扰进行倒推。然后,结合估计的干扰值,利用 Lyapunov 理论设计出分布式自适应编队控制器。它由与无人飞行器平移和旋转运动相关的位置控制器和姿态控制器组成。通过满足 Lyapunov 稳定函数的标准来验证稳定性。无人飞行器通过基于可变邻接矩阵的有向网络拓扑结构进行连接,并通过拉普拉斯矩阵的特性建立网络连接。通过对三角形、正方形、四面体、八面体和立方体等不同理想形状的严格模拟研究,证明了所设计控制器的鲁棒性。参考轨迹被视为螺旋形、直线形和圆形。外部时变干扰为不同幅度的正弦波。仿真结果表明,所提出的基于 RBFNN 的编队控制器可以往复处理不同的正弦波形,从而成功实现所需的编队。广泛的比较研究表明,针对不同形状的轨迹和所需队形,所提出的自适应队形控制器比文献中现有的控制器更有效。
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Adaptive neural network based quadrotor UAV formation control under external disturbances
The formation control of a team comprised of multiple quadrotor Unmanned Aerial Vehicles (UAVs) may severely be affected by the unknown external disturbances. The external disturbances are caused by wind forces to create aero-dynamical disturbances. This article addresses the robust formation control problem of multiple UAVs system despite the effect of external disturbances that allow sustaining a stable network connection among the UAVs and maintaining different formations assigned to them. First, a Radial Basis Function Neural Network (RBFNN) based model is developed to reciprocate the external disturbances along the positional and the attitude subsystems. Then incorporating the estimated disturbance values a distributed adaptive formation controller is devised using the Lyapunov theory. It consists of a positional and an attitude controller associated with the translational and the rotational movements of the UAVs. The stability is validated by satisfying the criteria of the Lyapunov stability function. The UAVs are connected through variable adjacency matrix based directed network topology and the network connectivity is established through the properties of the Laplacian Matrix. The robustness of the designed controller is justified via rigorous simulation studies for different sets of desired formations such as triangular, squared, tetrahedron, octahedron and cube shaped. The reference trajectories are considered as spiral, straight line and circular shaped. The time varying external disturbances are considered of sinusoidal waveform of different magnitudes. The simulation results signifies that the proposed RBFNN based formation controller reciprocate different sinusoidal waveforms to achieve the desired formations successfully. Extensive comparative studies demonstrate the efficacy of the proposed adaptive formation controller over the existing controllers presented in the literature for different shapes of trajectories and desired formations.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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