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首页> 外文期刊>International Journal of Adaptive Control and Signal Processing >Robust adaptive constrained boundary control for a suspension cable system of a helicopter
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Robust adaptive constrained boundary control for a suspension cable system of a helicopter

机译:直升机悬索系统的鲁棒自适应约束边界控制

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摘要

In this article, the problems of modeling and controlling are investigated for a suspension cable system of a helicopter with input saturation, system parameter uncertainties, and external disturbances by using the boundary control method. In accordance with the Hamilton's principle, the model of the suspension cable system of a helicopter is established by using a set of partial differential and ordinary differential equations. Considering nonsymmetric saturation constraint, the auxiliary systems are designed to handle with the effect of input saturation. Considering Lyapunov's direct method and the designed auxiliary systems, two robust adaptive boundary controllers are provided by the actuators at the helicopter and the box. Under the proposed controllers, the error between the bottom payload and the target location and the vibration range are uniformly ultimately bounded. Moreover, they will converge to a small neighborhood of zero by selecting the suitable parameters. Meanwhile, to guarantee the validity of the proposed adaptive boundary control laws, some sufficient conditions are raised. Simulation results are provided to verify that the effectiveness of the designed controllers in this paper.
机译:本文利用边界控制方法研究了具有输入饱和,系统参数不确定性和外部干扰的直升机悬索系统的建模和控制问题。根据汉密尔顿原理,通过使用一组偏微分方程和常微分方程建立直升机的悬索系统模型。考虑到非对称饱和约束,辅助系统设计用于处理输入饱和的影响。考虑到李雅普诺夫的直接方法和设计的辅助系统,直升飞机和行李箱上的执行器提供了两个鲁棒的自适应边界控制器。在所提出的控制器下,底部有效载荷与目标位置之间的误差以及振动范围最终均匀地受到限制。此外,通过选择合适的参数,它们将收敛到零的小邻域。同时,为保证所提出的自适应边界控制律的有效性,提出了一些充分的条件。提供仿真结果以验证本文设计的控制器的有效性。

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