四旋翼飞行器的二阶滑模控制

Sudhir, A. Swamp
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引用次数: 25

摘要

由于系统的高度非线性和外部干扰,四旋翼飞行器的模型是非线性的和动态不稳定的。针对四旋翼飞行器的高度跟踪问题,提出了一种鲁棒二阶滑模控制器。利用李雅普诺夫稳定性方法推导了控制器,并从理论上证明了控制器的渐近稳定性。通过与文献中的传统滑模控制进行比较,评价了所提控制方法的性能。结果表明,所提出的二阶滑模控制提高了跟踪控制性能,具有较好的暂态性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Second order sliding mode control for quadrotor
The model of a quadrotor is nonlinear and dynamically unstable due to the high level of system nonlinearity and external disturbances. In this paper a robust second order sliding mode controller has been proposed for altitude tracking of a quadrotor. The controller is derived using Lyapunov stability approach and proved theoretically asymptotic stability. The performance of proposed control method is evaluated by comparing the performance with conventional sliding mode control from the literature. It is demonstrate that the proposed second order sliding mode control improves the tracking control performance with better transient performances.
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