Identification of Aerodynamic Coefficients of Ground Vehicles Using Neural Network

N. Ramli, S. Mansor, H. Jamaluddin, W. Faris
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引用次数: 2

Abstract

The purpose of this paper is to demonstrate the application of a combination of neural network and an oscillating model facility as an approach in identification of aerodynamic coefficients of ground vehicle. In literature study, a method for estimating transient aerodynamic data has been introduced and the aerodynamic coefficients are extracted from the measured time response by means of conventional approach. The potential of neural network as an alternative method is explored. For simplicity, only the damped oscillation considered in this analysis while neglecting any unsteadiness or buffeting load Two feedforward neural networks are constructed to estimate the damping ratio and natural frequency, respectively, from the measured time response recorded during the dynamic wind tunnel test. These two parameters are used to calculate the aerodynamic coefficients of the ground vehicle model. To validate the network approach, the resulted coefficients are compared with the ones retrieved conventionally. By simulating the system's transfer function, the response generated from neural network results were found to be closer to the measured time response compared to the response generated using the conventionally estimated coefficients.
基于神经网络的地面车辆气动系数辨识
本文的目的是演示神经网络与振动模型装置相结合的方法在地面飞行器气动系数识别中的应用。在文献研究中,引入了一种估算瞬态气动数据的方法,并采用常规方法从测量的时间响应中提取气动系数。探讨了神经网络作为一种替代方法的潜力。为简单起见,本分析中只考虑阻尼振荡,忽略非定常或抖振载荷,构建两个前馈神经网络,分别从动力风洞试验中记录的实测时间响应估计阻尼比和固有频率。这两个参数用于计算地面飞行器模型的气动系数。为了验证网络方法,将得到的系数与常规检索的系数进行了比较。通过模拟系统的传递函数,发现与使用常规估计系数产生的响应相比,由神经网络结果产生的响应更接近于测量时间响应。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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