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Robustness analysis of fractional order PID for an electrical aerial platform

机译:电气平台小数PID的鲁棒性分析

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This work was performed to objectively measure and assess the robustness and tracking performance of fractional order of proportional, integral and derivative (FOPID) controller as compared to the conventional PID control. In satellite research and development, the satellite undergoes numerous tests such as thermal, acoustic and vibration tests in the cleanroom environment. However, due to space limitation in the cleanroom and the sensitive components of the satellite, it requires vibration-free, smooth and precise motion when handling the satellite. In addition, measurement interference might occur due to cable routing during procedures or tasks performed by an operator. Unlike the previous work, the robustness analysis of FOPID controller was not systematically conducted. In this paper, the analysis took into account the actuator dynamics, and various tests were considered to measure the robustness of FOPID controller. The designed FOPID controller was implemented on the scissor-type lifting mechanism of motorized adjustable vertical platform (MAVeP) model, and its performance was compared with the traditional PID controller. A comprehensive verification using MATLAB and Solidworks was carried out to generate the model and conduct the analysis. Both controllers were initially tuned using Nichol-Ziegler technique, and the additional FOPID controller parameters was tuned using the Astrom-Hagglund method. From the simulation work, it was found that the FOPID controller's tracking error was reduced between 10 % - 50 % for the disturbance rejection tests and reference to disturbance ratio (RDR) spectrum was higher as compared to PID. The analysis in this paper was predicted to be the main driver to implement FOPID controller in the complex system in the industry, especially for sensitive material handling and transportation such as satellite.
机译:与传统PID控制相比,执行此工作以客观地测量和评估比例,积分和衍生物(FoPID)控制器的分数顺序的鲁棒性和跟踪性能。在卫星研发中,卫星在洁净室环境中经历了许多试验,如热,声学和振动试验。然而,由于洁净室中的空间限制和卫星的敏感部件,在处理卫星时需要无振动,光滑和精确的运动。此外,由于操作员执行的过程或任务期间电缆路由,可能发生测量干扰。与以前的工作不同,未经系统地进行FoPID控制器的稳健性分析。在本文中,分析考虑了执行器动力学,并考虑了各种测试来测量FoPID控制器的稳健性。设计的FOPID控制器在电动可调节垂直平台(MAVEP)型号的剪刀式提升机构上实现,其性能与传统的PID控制器进行了比较。进行了使用MATLAB和SOLIDWORKS的全面验证以产生模型并进行分析。两个控制器最初使用Nichol-Ziegler技术进行调整,并且使用astrom-hagglund方法进行额外的FoPID控制器参数。从仿真工作来看,发现FoPID控制器的跟踪误差在10% - 50%之间减少到干扰抑制试验的10% - 50%之间,与PID相比,对干扰比(RDR)谱的参考较高。本文的分析预计是在行业中实现FoPID控制器的主要驱动器,特别是对于诸如卫星等敏感材料处理和运输。

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