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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Trajectory tracking of a quadrotor with unknown parameters and its fault-tolerant control via sliding mode fault observer
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Trajectory tracking of a quadrotor with unknown parameters and its fault-tolerant control via sliding mode fault observer

机译:参数未知的四旋翼的轨迹跟踪及其通过滑模故障观测器的容错控制

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摘要

Based on the nonlinear equations of a quadrotor, position tracking with unknown parameters and fault-tolerant control scheme is proposed in this article. First, a multi-loop structure is designed with multiple time-scale analysis to make the system realizable. Then, to achieve the goal of accurate tracking, a sliding mode fault observer is added into each loop to accommodate the effects of all the uncertainties. This controller shows great applicability because of the simple structure. The only information the controller needs to know is the limits of uncertainties. In addition, since the above controller cannot guarantee robustness when the system model is unknown, an online adaptive estimation method is proposed to learn the parameter information. Stability of the overall closed-loop system is analyzed with the Lyapunov stability theory, and output tracks the expected trajectory. The simulation is presented with several situations (including adaptive estimation result test/robust test under parameter uncertainties and high-frequency noise/fault-tolerant ability under actuator faults) to verify the effectiveness and feasibility of the proposed scheme.
机译:基于四旋翼飞机的非线性方程,提出了未知参数的位置跟踪和容错控制方案。首先,设计了具有多个时间尺度分析的多回路结构,以使系统可实现。然后,为了达到精确跟踪的目的,将滑模故障观测器添加到每个循环中以适应所有不确定性的影响。由于结构简单,该控制器显示出极大的适用性。控制器需要知道的唯一信息是不确定性的限制。另外,由于上述控制器在系统模型未知时不能保证鲁棒性,因此提出了一种在线自适应估计方法来学习参数信息。使用Lyapunov稳定性理论分析了整个闭环系统的稳定性,并且输出跟踪了预期的轨迹。在几种情况下进行了仿真(包括参数不确定性下的自适应估计结果测试/鲁棒性测试以及执行器故障下的高频噪声/容错能力),以验证该方案的有效性和可行性。

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