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Guidance-Error-Based Robust Fuzzy Adaptive Control for Bottom Following of a Flight-Style AUV With Saturated Actuator Dynamics

机译:具有饱和执行器动态的飞行式AUV的底部的指导误差的鲁棒模糊自适应控制

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This paper addresses the problem of robust bottom following control for a flight-style autonomous underwater vehicle (AUV) subject to system uncertainties, actuator dynamics, and input saturation. First, the actuator dynamics that is approximated by a first-order differential equation is inserted into the AUV dynamics model, which renders a high-order nonlinear dynamics analysis and design in the model-based backstepping controller by utilizing guidance errors. Second, to overcome the shaking control behavior resulted by the model-based high-order derivative calculation, a fuzzy approximator-based model-free controller is proposed, in order to online approximate the unknown part of the ideal backstepping architecture. In addition, the adaptive error estimation technology is resorted to compensate the system approximation error, ensuring that all the position and orientation errors of robust bottom following control tend to zero. Third, to further tackle the potential unstable control behavior from inherent saturation of control surfaces driven by rudders, an additional adaptive fuzzy compensator is introduced, in order to compensate control truncation between the unsaturated and saturation inputs. Subsequently, Lyapunov theory and Barbalat lemma are adopted to synthesize asymptotic stability of the entire bottom following control system. Finally, comparative numerical simulations with different controllers, environmental disturbances and initial states are provided to illustrate adaptability and robustness of the proposed bottom following controller for a flight-style AUV with saturated actuator dynamics.
机译:本文解决了通过系统不确定性,执行器动力学和输入饱和度的飞行式自主水下车辆(AUV)控制的强大底部的问题。首先,将由一阶微分方程近似的致动器动力学被插入AUV动力学模型,该模型通过利用引导误差来使基于模型的BackStepping控制器中的高阶非线性动态分析和设计。其次,为了克服基于模型的高阶导数计算导致的振荡控制行为,提出了一种基于模糊的近似器的无模型控制器,以便在线近似理想的反向架构的未知部分。此外,采用自适应误差估计技术补偿了系统近似误差,确保了鲁棒底部的所有位置和方向误差趋于为零。第三,为了进一步解决来自舵机驱动的控制表面的固有饱和的潜在不稳定的控制行为,引入了另外的自适应模糊补偿器,以补偿不饱和和饱和输入之间的控制截断。随后,采用Lyapunov理论和Barbalat Lemma合成整个底部后控制系统的渐近稳定性。最后,提供了具有不同控制器,环境干扰和初始状态的比较数值模拟,以说明具有饱和执行器动态的飞行式AUV的所提出的底部控制器的适应性和鲁棒性。

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