约束四旋翼飞行器轨迹跟踪的自适应积分滑模控制

Khelil Sidi Brahim, A. Hajjaji, N. Terki, D. L. Alabazares
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引用次数: 0

摘要

研究了未知上界扰动下四旋翼飞行器的约束位置和角度跟踪控制设计。提出了一种自适应积分滑模控制(AISMC),用于四旋翼飞行器在严重干扰和输入饱和约束下的位置和角度跟踪。所提出的方法不需要对干扰边界的先验知识,允许通过自适应动态律来减少计算工作量,获得良好的跟踪,并避免对自动处理输入饱和约束的模态滑动增益的高估。用李亚普诺夫理论证明了该算法在有限时间内的稳定性和收敛性。仿真结果表明了该方法的有效性
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Adaptive Integral Sliding Mode Control for Constrained Quadrotor Trajectory Tracking
This paper deals with the constrained position and angle tracking control design for quadrotor under unknown upper bound disturbances. An adaptive integral sliding mode control (AISMC) is proposed to perform the position and angle tracking for the quadrotor subject the severe disturbances and input saturation constraints. The proposed approach that does not require a priori knowledge of disturbance boundaries, allows through an adaptation dynamic law to reduce the computing effort, to obtain a good tracking, and to avoid an overestimation of the gain of the mode sliding that will automatically handle input saturation constraints. Stability and convergence in finite time are proved by Lyapunov theory. The efficiency of the proposed method is shown by simulation
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