首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Virtual guidance-based finite-time path-following control of underactuated autonomous airship with error constraints and uncertainties
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Virtual guidance-based finite-time path-following control of underactuated autonomous airship with error constraints and uncertainties

机译:基于虚拟的指导的有限时间路径跟踪欠抖动自治飞艇的控制,具有错误约束和不确定性

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摘要

This paper addresses the finite-time three-dimensional path-following control problem for underactuated autonomous airship with error constraints and uncertainties. First, a five degrees-of-freedom path-following error model in the Serret-Frenet coordinate frame is established. By applying the finite-time stability theory, a virtual guidance-based finite-time adaptive neural backstepping path-following control approach is proposed. Barrier Lyapunov functions (BLFs) are introduced to deal with attitude error constraints. Neural networks (NNs) are presented to compensate for the uncertainties. To prevent the "explosion of complexity" in the design of the backstepping method, a finite-time convergent differentiator (FTCD) is introduced to estimate the time derivatives of virtual control signals. Stability analysis showed that all closed-loop signals are uniformly ultimately bounded, the constrained requirements on the airship attitude errors are never violated, and the path-following errors converge to a small neighborhood of the origin in a finite time. At last, simulation studies are provided to demonstrate the effectiveness of the proposed control approach.
机译:本文涉及欠限制和不确定性的欠抗动自动飞艇的有限时间三维路径控制问题。首先,建立了SLET-FRENET坐标帧中的五个自由度路径误差模型。通过应用有限时间稳定性理论,提出了一种基于虚拟指导的有限时间自适应神经背杆PATH-之后的控制方法。屏障Lyapunov功能(BLF)被引入处理态度误差约束。提出神经网络(NNS)以补偿不确定性。为了防止“复杂性的爆炸”在反静电方法的设计中,引入了有限时间的会聚微分器(FTCD)来估计虚拟控制信号的时间衍生物。稳定性分析表明,所有闭环信号都是均匀的最终界限,对飞艇姿态误差的受约束要求永远不会违反,并且路径误差在有限时间内收敛到原点的小邻域。最后,提供了仿真研究以证明所提出的控制方法的有效性。

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