首页> 外文会议>AHS 59th Annual Forum Proceedings Vol.2; May 6-8, 2003; Phoenix, Arizona >Identification of Helicopter Dynamics based on Flight Data using Recurrent Neural Networks: A Comparative Study
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Identification of Helicopter Dynamics based on Flight Data using Recurrent Neural Networks: A Comparative Study

机译:基于飞行数据的递归神经网络直升机动力学识别的比较研究

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In this paper, we present a comparative analysis of different artificial neural networks (ANN) for identification of longitudinal and lateral dynamics of helicopter using flight data. These methods have an advantage over the traditional methods for identification because the model structure need not be defined apriori. In case of helicopter dynamics, defining apriori model is difficult because of highly nonlinear aeromechanical characteristics due to the interplay between various subsystems like rotor, fuselage, power plant, transmission, empennage, and tail rotor. For a given input-output data set, ANN's are capable of fully capturing the underlying relationship. Three different ANN architectures namely, Non-linear Auto Regressive exogenous input (NARX) model, ANN with internal memory known as Memory Neuron Networks (MNN) and Recurrent MultiLayer Perceptron (RMLP) networks have been used to identify longitudinal and lateral dynamics of the helicopter at various speeds. Actual flight data are used for simulation studies that are carried out using various ANN architectures and their performances are compared. Based on the identification results, the practical utility, advantages and limitations of the three models are critically appraised.
机译:在本文中,我们对使用飞行数据识别直升机纵向和横向动力学的不同人工神经网络(ANN)进行了比较分析。与传统的识别方法相比,这些方法具有优势,因为无需事先定义模型结构。在直升机动力学的情况下,由于高度非线性的航空机械特性(如旋翼,机身,动力装置,变速器,尾翼和尾桨)之间的相互作用,很难定义先验模型。对于给定的输入输出数据集,ANN能够完全捕获基础关系。三种不同的ANN架构,即非线性自动回归外源输入(NARX)模型,具有内部记忆的ANN(称为记忆神经元网络(MNN)和递归多层感知器(RMLP)网络)已用于识别直升机的纵向和横向动态以各种速度。实际的飞行数据用于使用各种ANN架构进行的模拟研究,并对它们的性能进行比较。根据识别结果,对三种模型的实用性,优点和局限性进行了严格评估。

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