利用屏障 Lyapunov 函数实现多架四旋翼飞行器系统的分布式安全编队跟踪控制

Nargess Sadeghzadeh-Nokhodberiz, Mohammad Reza Sadeghi, Rohollah Barzamini, Allahyar Montazeri
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引用次数: 0

摘要

使用基于共识的技术协调机器人群的运动,是实现特定任务预期目标的一个重要问题。虽然现有的大多数基于共识的控制技术都忽略了机器人在瞬态阶段的碰撞问题,但这些技术要么计算成本高昂,要么无法应用于有动态障碍物的环境。因此,我们利用障碍李亚普诺夫函数(BLF)的特性,为多四轴飞行器系统提出了一种新的分布式无碰撞编队跟踪控制方案。因此,我们将问题置于反步态环境中,并推导出一种能保证四旋翼无碰撞编队跟踪的分布式控制法则。换句话说,使用所提出的位置子系统 BLF,可以在预定的精度下同时解决跟踪和避免代理间碰撞的问题,并通过二次 Lyapunov 函数的增强来设计控制器。由于四旋翼飞行器系统的欠驱动性质,平移(X 轴和 Y 轴)子系统考虑了虚拟控制输入,然后利用虚拟控制输入为姿态控制子系统生成所需的滚动角和俯仰角值。这就为每架四旋翼飞行器提供了一个分层控制器结构。每架四旋翼飞行器的姿态控制器都是根据另一个 BLF 的预定误差限制进行本地设计的。最后,提供了 MATLAB-Simulink 环境下的仿真结果,以显示所提方法的准确性。还提供了与基于优化的技术的数值比较,以证明所提方法在计算成本、稳态误差和响应时间方面的优越性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Distributed safe formation tracking control of multiquadcopter systems using barrier Lyapunov function
Coordinating the movements of a robotic fleet using consensus-based techniques is an important problem in achieving the desired goal of a specific task. Although most available techniques developed for consensus-based control ignore the collision of robots in the transient phase, they are either computationally expensive or cannot be applied in environments with dynamic obstacles. Therefore, we propose a new distributed collision-free formation tracking control scheme for multiquadcopter systems by exploiting the properties of the barrier Lyapunov function (BLF). Accordingly, the problem is formulated in a backstepping setting, and a distributed control law that guarantees collision-free formation tracking of the quads is derived. In other words, the problems of both tracking and interagent collision avoidance with a predefined accuracy are formulated using the proposed BLF for position subsystems, and the controllers are designed through augmentation of a quadratic Lyapunov function. Owing to the underactuated nature of the quadcopter system, virtual control inputs are considered for the translational (x and y axes) subsystems that are then used to generate the desired values for the roll and pitch angles for the attitude control subsystem. This provides a hierarchical controller structure for each quadcopter. The attitude controller is designed for each quadcopter locally by taking into account a predetermined error limit by another BLF. Finally, simulation results from the MATLAB-Simulink environment are provided to show the accuracy of the proposed method. A numerical comparison with an optimization-based technique is also provided to prove the superiority of the proposed method in terms of the computational cost, steady-state error, and response time.
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