四旋翼飞行器非线性轨迹跟踪控制的分析动力学方法:数值与实验结果

P. Souza, K. Stol
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引用次数: 1

摘要

本文提出了一种基于解析动力学和四元数理论的四旋翼无人机非线性轨迹跟踪控制方法。将受约束机械系统的运动方程重新解释为得到显式非线性控制律的解。此外,通过对模拟结果和实验结果进行定性和定量比较,研究了实际控制方面和非理想性的影响。数值仿真结果表明,所提出的控制器能够以很小的跟踪误差跟踪目标轨迹,无论是简单轨迹还是剧烈轨迹。使用通用的开源解决方案,讨论了控制方法的实际实现可行性、性能和局限性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
An Analytical Dynamics Approach for Nonlinear Trajectory-Tracking Control of Quadrotors: Numerical and Experimental Results
This paper presents an alternative approach for nonlinear trajectory-tracking control of quadrotor unmanned aerial vehicles (UAVs) based on analytical dynamics and quaternion theories. The equations of motion of constrained mechanical systems are reinterpreted as a solution for obtaining an explicit nonlinear control law. In addition, practical control aspects and the impact of nonidealities are investigated by providing qualitative and quantitative comparisons between simulated and experimental results. Numerical simulations demonstrate the efficacy of the proposed controller to track desired trajectories with very small tracking error for simple as well as aggressive or sharp trajectories. Using common open-source solutions, real-world implementation feasibility, performance, and limitations of the control method are discussed.
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