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Harmonic Extended State Observer Based Anti-Swing Attitude Control for Quadrotor with Slung Load

机译:基于谐波扩展状态观测器的摆臂四旋翼防摆姿态控制

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During the flight of the quadrotor, the existence of a slung load will exert a swing effect on the system and the motion of which will significantly change the dynamics of the quadrotor. The external torque caused by the slung load can be considered as a kind of disturbance and it is a threat to the attitude control stability of the system. In order to solve this problem, a high precision disturbance compensation method is presented in this paper, based on the harmonic extended state observer (HESO). Firstly, a generic mathematical model for the quadrotor-slung load system is obtained via the Lagrangian mechanics, and according to the analysis of the slung load motion, we obtain the disturbance as a form of periodic equation. Secondly, based on the dynamic model of the disturbance, we propose a HESO to achieve high precision disturbance estimation and its stability is proved by Lyapunov theory. Thirdly, we designed an attitude tracking controller based on backstepping method, and discussed the stability of the entire system. Finally, numerical simulations and real time experiments are carried out to evaluate the performance of the proposed method. Our results show that the robustness of the quadrotor subject to slung load has been improved.
机译:在四旋翼飞行期间,倾斜负载的存在将对系统产生摆动效应,其运动将显着改变四旋翼的动力学。由倾斜负载引起的外部转矩可以被认为是一种干扰,它威胁着系统的姿态控制稳定性。为了解决这个问题,本文提出了一种基于谐波扩展状态观测器(HESO)的高精度干扰补偿方法。首先,通过拉格朗日力学,建立了四旋翼-甩负荷系统的通用数学模型,并通过对甩负荷运动的分析,得到了周期方程形式的扰动。其次,基于扰动的动力学模型,提出了一种能实现高精度扰动估计的HESO,并通过Lyapunov理论证明了其稳定性。第三,设计了一种基于后推法的姿态跟踪控制器,并讨论了整个系统的稳定性。最后,通过数值模拟和实时实验来评估该方法的性能。我们的结果表明,四轴转子承受斜载的鲁棒性得到了提高。

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