多旋翼机智能跟踪控制的实训仿真结合平台

Mohammad Bajelani, Morteza Tayefi, Man Zhu
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引用次数: 3

摘要

目的为降低飞行试验在轨迹跟踪控制设计过程中出现的昂贵失败风险,提出了一种将整个飞行器置于仿真回路的方法。多旋翼无人机的智能控制器和数据驱动控制器的开发离不开实际系统,需要了解无人机的非线性复杂动力学特性。本文提出的车辆在环平台是解决这一问题的一种安全有效的方法。设计/方法/方法为了在控制器设计过程中避免危险的飞行试验,多旋翼铰接在一个轴上,该轴允许多旋翼的角运动,但限制了平移运动。该试验台包括真实系统姿态动力学和位置动力学仿真两部分,基于飞行器的实时反应对整个飞行过程进行建模。以六自由度飞行器的角运动为例,在平动仿真回路中提供实时姿态数据。为了验证该设置,实现了比例-积分-导数(PID)和基于大脑情绪学习的智能控制器(BELBIC),用于跟踪圆形和8形飞行轨迹。研究结果表明,该平台可以帮助智能控制器在设计初期和实际飞行试验中无需担心故障的情况下学习系统动力学。虽然在仿真中对六旋翼机的平移动力学进行了建模,但作者仍然具有与控制回路设计要求相匹配的高精度姿态动力学。两种控制器的对比也表明,在本次测试中,BELBIC的性能优于PID。原创性/价值引言部分回顾了研究背景。其他部分最初是在本文中开发的。
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A real-test and simulation combined platform for developing intelligent tracking control of multirotors
PurposeThis study aims to minimize the risk of costly failures of flight tests during the path tracking control design, and a noble approach has been proposed in this study to put the whole vehicle-in-the simulation loop. Working with the real system is essential for developing intelligent and data-driven controllers for multirotor drones which needs learning the drones' nonlinear complicated dynamics. The vehicle-in-the-loop (VIL) platform developed in this paper is a safe and effective solution to deal with this problem.Design/methodology/approachTo avoid risky flight test during controller design, the multirotor is hinged to a shaft that allows the multirotor's angular motion but restricts translational motion. The test-bed includes the real system attitude dynamics and the simulation of the position dynamics to model the complete flight based on real-time reactions of the vehicle. For the authors' case study, a hexacopter angular motion provides the real-time attitude data in translational motion simulation loop. To test the set-up, a proportional-integral-derivative (PID) and a brain emotional learning-based intelligent controller (BELBIC) is implemented for tracking of circle and 8-shape flight trajectories.FindingsThe results show that the platform helps the intelligent controller to learn the system dynamics without worrying about the failure in the early stages of the design and in the real-world flight test. Although the hexacopter translational dynamics is modeled in simulation, the authors still have highly accurate attitude dynamics matching the requirement of the control loop design. The comparison of the two controllers also shows that the performance of BELBIC is better than PID in this test.Originality/valueThe research background is reviewed in the introduction section. The other sections are originally developed in this paper.
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CiteScore
3.50
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0.00%
发文量
21
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