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Input-output tracking control of a 2-DOF laboratory helicopter with improved algebraic differential estimation

机译:具有改进的代数差分估计的2-DOF实验室直升机的输入-输出跟踪控制

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This paper presents a study on input-output feedback linearization control (OFLC) of a laboratory twin rotor helicopter system based on an improved algebraic differential estimation approach. In the previous algebraic differential estimation studies, the reset time T-r is always selected cautiously in a narrow range because the estimation accuracy is very sensitive to T-r. Too small or too large reset time T-r will lead to an inaccurate estimation of signal derivatives. In this paper, we first propose a new resetting and overlapping strategy for improving the robustness of the estimation algorithm. Then it is used to estimate the velocities of pitch and yaw motions. The OFLC is designed and verified by letting the output signals track different periodic reference signals. Both simulation and experimental results show better control performance as compared with the LQR design. (C) 2018 Elsevier Ltd. All rights reserved.
机译:本文提出了一种基于改进的代数差分估计方法的实验室双旋翼直升机系统的输入输出反馈线性化控制(OFLC)的研究。在先前的代数差分估计研究中,重置时间T-r总是在狭窄的范围内谨慎选择,因为估计精度对T-r非常敏感。重置时间T-r太小或太大都会导致信号导数的估计不准确。在本文中,我们首先提出一种新的重置和重叠策略,以提高估计算法的鲁棒性。然后用于估计俯仰和偏航运动的速度。通过让输出信号跟踪不同的周期性参考信号来设计和验证OFLC。与LQR设计相比,仿真和实验结果均显示出更好的控制性能。 (C)2018 Elsevier Ltd.保留所有权利。

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