Adaptive robust sliding mode controller design for full control of quadrotor with external disturbances

Alireza Modirrousta, M. Khodabandeh
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引用次数: 18

Abstract

This paper proposes two different adaptive robust sliding mode controllers for attitude, altitude and position control of a quadrotor. First it proposes a backstepping non-singular terminal sliding mode control with adaptive algorithm which applied to the quadrotor for free chattering, finite time convergences and robust aims. In this control scheme instead of regular control input, the derivative of the control input is achieved from non-singular terminal second-layer sliding surface. And an adaptive tuning method is utilized to deal with the external disturbances whose upper bounds are not required to be known in advance in the inner loop. Second nonlinear disturbance observer based on integral sliding mode with adaptive gains is proposed for position control which is known as outer loop. Stability and robustness of the proposed controller are proved by using the classical Lyapunov criterion. The simulation results demonstrate the validation of the proposed control scheme.
具有外部扰动的四旋翼飞行器的自适应鲁棒滑模控制器设计
针对四旋翼飞行器的姿态、高度和位置控制,提出了两种不同的自适应鲁棒滑模控制器。首先提出了一种基于自适应算法的反步非奇异末端滑模控制方法,该方法适用于四旋翼飞行器,具有自由抖振、有限时间收敛和鲁棒性。该控制方案取代常规控制输入,从非奇异终端第二层滑动面对控制输入求导。采用自适应调谐方法处理内环中不需要事先知道上界的外部扰动。提出了一种基于自适应增益的积分滑模非线性扰动观测器,用于外环位置控制。利用经典的李雅普诺夫准则证明了该控制器的稳定性和鲁棒性。仿真结果验证了所提控制方案的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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