四旋翼无人机仿生反步滑模控制与自适应滑模创新滤波器

Zhe Xu , Tao Yan , Simon X. Yang , S. Andrew Gadsden
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引用次数: 0

摘要

四旋翼无人机是近年来应用最广泛的飞行机器人。本文将反步滑模控制技术与仿生神经动力学模型相结合,提出了一种仿生控制策略。本文讨论了扰动、系统噪声和测量噪声对四旋翼无人机控制性能的影响。所提出的控制策略对扰动具有鲁棒性,并通过李雅普诺夫稳定性理论证明了其稳定性。此外,所提出的控制策略能够在噪声下提供平滑的控制输入。考虑到建模的不确定性,将自适应滑动创新滤波器与所提出的控制相结合,以提供准确的状态估计,从而提高跟踪效果。最后,仿真结果表明,所提出的控制策略为在干扰和噪声下运行的四旋翼无人飞行器提供了令人满意的跟踪性能。
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Bioinspired backstepping sliding mode control and adaptive sliding innovation filter of quadrotor unmanned aerial vehicles

Quadrotor unmanned aerial vehicles have become the most commonly used flying robots with wide applications in recent years. This paper presents a bioinspired control strategy by integrating the backstepping sliding mode control technique and a bioinspired neural dynamics model. The effects of both disturbances and system and measurement noises on the quadrotor unmanned aerial vehicle control performance have been addressed in this paper. The proposed control strategy is robust against disturbances with guaranteed stability proven by the Lyapunov stability theory. In addition, the proposed control strategy is capable of providing smooth control inputs under noises. Considering the modeling uncertainties, the adaptive sliding innovation filter is integrated with the proposed control to provide accurate state estimates to improve tracking effectiveness. Finally, the simulation results demonstrate that the proposed control strategy provides satisfactory tracking performance for a quadrotor unmanned vehicle operating under disturbances and noises.

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