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Trajectory tracking for two-degree of freedom helicopter system using a controller-disturbance observer integrated design

机译:使用控制器扰动观测器综合设计的二维自由直升机系统的轨迹跟踪

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摘要

Trajectory tracking control for helicopters, which are widely used in severe situations such as military and rescue missions, is a challenging field of research. In helicopter system, the stability problem and predefined trajectories tracking are main challenges, especially in the presence of external disturbances and dynamic model uncertainties. Hence, a robust control design is needed for tracking the desired references. There has been a lot of motivation for solving these problems with simpler methods and also reducing the couplings in the helicopter system to achieve better performance, as the presented paper attempts to fill these gaps. This paper focuses on designing control laws for two-degree of freedom helicopter system while assuring the closed-loop stability. A nonlinear disturbance observer-based control (NDOBC) is designed for attenuating the effects of exogenous disturbances. Trajectory tracking controller and nonlinear disturbance observer are formulated in the form of two linear matrix inequality (LMI) problems. The closed-loop system stability, including controller and observer, is investigated by Lyapunov theorem. The effectiveness of the proposed design for tracking the trajectories (vertical flight and pitch angle rotor blade) and disturbance estimation is verified by simulation results. (C) 2018 ISA. Published by Elsevier Ltd. All rights reserved.
机译:用于直升机的轨迹跟踪控制,广泛用于军事和救援任务等严峻局势,是一个具有挑战性的研究领域。在直升机系统中,稳定性问题和预定义的轨迹跟踪是主要挑战,特别是在存在外部干扰和动态模型的不确定性。因此,需要一种鲁棒的控制设计来跟踪所需的参考。通过更简单的方法解决这些问题以及降低直升机系统的联轴器,以实现更好的性能,因此有很多动力,因为所提出的纸张试图填补这些空隙。本文侧重于设计两级自由直升机系统的控制法,同时确保闭环稳定性。基于非线性干扰观察者的控制(NDOBC)设计用于减弱外源干扰的影响。轨迹跟踪控制器和非线性干扰观测器以两个线性矩阵不等式(LMI)问题的形式配制。 Lyapunov定理研究了闭环系统稳定性,包括控制器和观察者。通过模拟结果验证了跟踪轨迹(垂直飞行和俯仰角转子叶片)和干扰估计的提出设计的有效性。 (c)2018 ISA。 elsevier有限公司出版。保留所有权利。

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