基于扩展状态观测器的四转子传递未知时变有效载荷的预测控制

Yuanyuan Wang
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引用次数: 0

摘要

研究了带有未知时变载荷的四旋翼飞行器的鲁棒控制问题。首先,建立了四旋翼飞行器载荷模型。将载荷的动力学作为扰动加入到四旋翼模型中。其次,为了增强系统的鲁棒性,采用扩展状态观测器(ESO)估计载荷扰动进行反馈补偿。然后,针对多输入多输出(MIMO)系统,提出了一种预测控制器,以降低载荷突然变化对系统的影响。最后,通过与传统的级联比例-积分-导数(CPID)和滑模控制(SMC)方法的比较,验证了所提出方案的优越性。仿真结果表明,CPID方法在姿态稳定方面表现出较差的性能,而SMC即使能达到满意的控制性能,也存在输入抖振现象。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Predictive Control of Quad-Rotor Delivering Unknown Time-Varying Payloads Based upon Extended State Observer
In this paper, robust control problem is addressed for quad-rotor delivering unknown time-varying payloads. Firstly, the model of a quad-rotor carrying payloads is built. Dynamics of the payloads are treated as disturbances and added into the model of the quad-rotor. Secondly, to enhance system robust-ness, the extended state observer (ESO) is applied to estimate the disturbances from the payloads for feedback compensation. Then a type of predictive controller targeting multiple-input-multiple-output (MIMO) system is developed to degrade the influences caused by sudden changes from load-ing/dropping of the payloads. Finally, by making comparison with the con-ventional cascade proportional-integral-derivative (CPID) and the sliding mode control (SMC) approaches, superiority of the scheme developed is va-lidated. The simulation results indicate that the CPID method shows poor performance on attitude stabilization and the SMC shows input chattering phenomenon even it can achieve satisfied control performances.
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