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Méthodologie de modélisation des systèmes mécatroniques complexes à partir du multi-bond graph : application à la liaison BTP-fuselage d’un hélicoptère

机译:从多键图建模复杂机电系统的方法论:在直升机的建造-机身连接中的应用

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摘要

Due to the operation of the rotor, the helicopter is subject to important vibrations affecting namely the fatigue of mechanical parts and the passengers comfort. The MGB-Fuselage joint equipped with the DAVI system is an anti-vibration system that helps to reduce, in a single frequency way, vibrations transmitted to the fuselage. Semi-active intelligent solutions are studied so that the filtering can be adjusted according to the vibration sources. Such studies suffer from a lack of tools and necessary methods, firstly, for the design of complex mechanical systems and secondly, for the development of an intelligent joint. This work proposes a modeling approach using a structural modeling tool : the multi-bond graph (MBG) which offers a global and modular view for the study of complex mechatronic systems such as helicopter. At first, an analysis of modeling tools leading to the selection of MBG is presented. Secondly, developments have focused on the MBG modeling of the 3D MGB-fuselage joint of an experimental setup which was designed and built in the laboratory. This joint is a mechanical system with kinematic loops. The equations of the dynamics of such system are a differential-algebraic system (DAE) requiring specific solving methods. The MBG model of the MGB-fuselage was simulated using the 20-sim software. The results were verified using the multibody software LMS Virtual Lab. A comparison of results obtained by the two methods led to a very good correlation to various cases of excitations of the MGB (pumping, roll, pitch). Thirdly, the MBG model was used for the establishment of semi-active control system. The model of the DAVI device also developed in 20-sim allows to adjust the position of the moving masses in operation so as to minimize the level of vibration of the fuselage. The control algorithm (gradient algorithm) enables to calculate the setpoint positions of the moving masses on the DAVI beaters. The position of the moving masses driven by an electric DC motor and a screw-nut system is then controlled to the setpoints generated by the control algorithm. Finally, the command could be implemented on a non-linear bond graph model which did not require a linearization to get a transfer function.
机译:由于旋翼的操作,直升机受到重要的振动影响,即机械零件的疲劳和乘客的舒适度。配备DAVI系统的MGB-机身接头是一种防振系统,有助于以单频方式减少传递到机身的振动。研究了半主动智能解决方案,以便可以根据振动源来调整滤波。此类研究缺乏工具和必要的方法,首先是复杂机械系统的设计,其次是智能关节的开发。这项工作提出了一种使用结构建模工具的建模方法:多键图(MBG),它为研究诸如直升机等复杂的机电系统提供了全局和模块化的视图。首先,对导致MBG选择的建模工具进行了分析。其次,开发集中在实验装置的3D MGB-机身接头的MBG建模上,该装置是在实验室设计和建造的。该关节是带有运动回路的机械系统。这种系统的动力学方程是需要特定求解方法的微分代数系统(DAE)。使用20-sim软件模拟了MGB机身的MBG模型。使用多体软件LMS Virtual Lab验证了结果。通过两种方法获得的结果的比较导致与MGB激励的各种情况(泵送,横摇,俯仰)有很好的相关性。第三,采用MBG模型建立了半主动控制系统。同样在20-sim中开发的DAVI设备的模型允许在运行中调整移动质量的位置,以使机身的振动程度最小化。控制算法(梯度算法)可以计算DAVI打浆机上移动质量的设定点位置。然后,将由直流电动机和螺母系统驱动的运动块的位置控制到由控制算法生成的设定点。最后,该命令可以在不需要线性化即可获得传递函数的非线性键合图模型上实现。

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    BOUDON Benjamin;

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  • 年度 2014
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  • 原文格式 PDF
  • 正文语种 fr
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