基于指数逼近律的无人机鲁棒轨迹跟踪

Saurabh Kumar, S. R. Kumar
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引用次数: 0

摘要

本文研究了无人机,特别是四旋翼飞行器的三维轨迹跟踪问题。首先,提出了一种基于时间尺度分离的双环层次控制设计。然后提出了一种渐近收敛的鲁棒非线性控制策略,利用滑模控制保证四旋翼飞行器的高精度轨迹跟踪。在该方法中,采用指数函数设计逼近律,该函数动态适应系统状态的变化,并保证四旋翼输入的抖振减小。通过仿真验证了该控制器在存在较大初始偏差和时变扰动的情况下的鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Exponential Reaching Law based Robust Trajectory Tracking for Unmanned Aerial Vehicles
This paper addresses the problem of three-dimensional trajectory tracking of unmanned aerial vehicles, specifically quadrotors. Firstly, a two-loop hierarchical control design is proposed based on the time scale separation. Then an asymptotically convergent robust nonlinear control strategy is proposed for both loops to ensure the quadrotor's high precision trajectory tracking using the sliding mode control. In this approach, the reaching law is designed using an exponential function that dynamically adapts to the variation of system states and ensures the chattering reduction in the quadrotor's inputs. The robustness of the proposed controller is tested in the presence of large initial deviations and time-varying disturbances using simulations.
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