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Identification of Helicopter Dynamics Based on Flight Data Using a PSO Driven Recurrent Neural Network Model

机译:PSO驱动的递归神经网络模型基于飞行数据的直升机动力学识别

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The complexity of helicopter flight dynamics makes modeling and helicopter system identification a very difficult task. Most of the traditional techniques used for nonlinear dynamical system identification require a model structure to be defined a priori. In case of helicopter dynamics, defining a priori model is difficult due to its complexity and the interplay between various subsystems. In this work we present a Particle Swarm Optimization (PSO) driven recurrent neural network model for the identification of helicopter dynamics using flight data, based on the popular Nonlinear Auto Regressive eXogeneous input network (NARX) model. The proposed model is capable of identifying the helicopter dynamics without any a. priori knowledge about the system under study. This model successfully circumvents one the major drawbacks of the very popular NARX model, without losing its numerous advantages. The current model is developed with the NARX model as the substrate; a single hidden layer perceptron network based architecture along with tapped delay lines is employed for modelling the dynamical systems. This is coupled with an II-Tier PSO-framework for evolving the order of the system. The model is used to approximate the flight data. Simulations have been carried out for identifying the longitudinally uncoupled dynamics. Results of identification indicate a quite close correlation between the actual and the predicted response of the helicopter. Further, the proposed model has been compared with the conventional NARX model.
机译:直升机飞行动力学的复杂性使建模和直升机系统识别成为一项非常困难的任务。用于非线性动力学系统识别的大多数传统技术都需要先验定义模型结构。在直升机动力学的情况下,由于先验模型的复杂性以及各个子系统之间的相互作用,很难定义先验模型。在这项工作中,我们基于流行的非线性自回归异质输入网络(NARX)模型,提出了一个由粒子群优化(PSO)驱动的递归神经网络模型,用于使用飞行数据识别直升机动力学。所提出的模型能够识别直升机动力而无需任何操作。有关正在研究的系统的先验知识。该模型成功地规避了非常流行的NARX模型的主要缺点之一,而又没有失去其众多优点。以NARX模型为基础开发当前模型;基于单个隐藏层感知器网络的体系结构以及抽头延迟线用于对动力学系统进行建模。这与II级Tier PSO框架结合在一起,用于发展系统的顺序。该模型用于近似飞行数据。为了识别纵向未耦合的动力学已经进行了仿真。识别结果表明,直升机的实际响应与预测响应之间存在非常密切的相关性。此外,已将提出的模型与常规的NARX模型进行了比较。

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