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用于非线性运动系统的切换步长积分反步控制及其在实验室直升机中的应用

Switched step integral backstepping control for nonlinear motion systems with application to a laboratory helicopter.

作者信息

Haruna A, Mohamed Z, Efe M Ö, Abdullahi A M

机构信息

Faculty of Electrical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia; Department of Mechatronics Engineering, Bayero University Kano, Nigeria.

Faculty of Electrical Engineering, Universiti Teknologi Malaysia, 81310 UTM Johor Bahru, Johor, Malaysia.

出版信息

ISA Trans. 2023 Oct;141:470-481. doi: 10.1016/j.isatra.2023.07.002. Epub 2023 Jul 4.

Abstract

In this paper, the energy efficiency of the widespread application of backstepping control to a class of nonlinear motion systems is investigated. A Switched Step Integral Backstepping Control (SSIBC) scheme is introduced to improve immunity to measurement noise and to increase the energy efficiency of conventional backstepping in practice. The SSIBC is realized by switching between two candidate controllers obtained at different steps of the iterative backstepping design process. A bi-state dependent hysteresis rule is developed to supervise stable switching between the different regimes in the presence of noise. The proposed method is experimentally verified on a MIMO twin rotor laboratory helicopter involving coupled nonlinear dynamics, inaccessible states and uncertainties. Experimental results show that in addition to a reduction in power consumption, the SSIBC reduces saturation of the control signal and visible motor jerking in contrast with conventional backstepping. Additional comparisons with a previously proposed optimized decoupling PID controller also show significant improvement in precision achieved with higher energy efficiency. Experimental results obtained with the introduction of an external disturbance into the system also show the robustness of the proposed SSIBC.

摘要

本文研究了反步控制在一类非线性运动系统中广泛应用的能量效率。引入了一种开关步积分反步控制(SSIBC)方案,以提高对测量噪声的免疫力,并在实际应用中提高传统反步控制的能量效率。SSIBC通过在迭代反步设计过程的不同步骤获得的两个候选控制器之间进行切换来实现。开发了一种双态相关滞后规则,以在存在噪声的情况下监督不同状态之间的稳定切换。该方法在一个涉及耦合非线性动力学、不可达状态和不确定性的多输入多输出双旋翼实验直升机上进行了实验验证。实验结果表明,与传统反步控制相比,SSIBC除了降低功耗外,还减少了控制信号的饱和以及明显的电机抖动。与先前提出的优化解耦PID控制器的额外比较也表明,在更高的能量效率下,精度有显著提高。在系统中引入外部干扰后获得的实验结果也表明了所提出的SSIBC的鲁棒性。

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