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Nonlinear identification of a small scale unmanned helicopter using optimized NARX network with multiobjective differential evolution

机译:基于多目标差分进化的优化NARX网络对小型无人直升机的非线性识别

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摘要

The need for a high fidelity model for design, analysis and implementation of an unmanned helicopter system (UHS) in various emerging civil applications cannot be underestimated. However, going by a first principle approach based on physical laws governing the dynamics of the system, this task is noted to be highly challenging due to the complex nonlinear characteristics of the helicopter system. On the other hand, the problem of determining network architecture for optimal/sub-optimal performances has been one of the major challenges in the use of the nonparametric approach based on Nonlinear AutoRegressive with exogenous inputs Network (NARX-network). The performance of the NARX network in terms of complexity and accuracy is largely dependent on the network architecture. The current approach in the literature has been largely based on trial and error, while most of the reported optimization approaches have limited the domain of the problem to a single objective problem. This study proposes a hybrid of conventional back propagation training algorithm for the NARX network and multiobjective differential evolution (MODE) algorithm for identification of a nonlinear model of an unmanned small scale helicopter from experimental flight data. The proposed hybrid algorithm was able to produce models with Pareto-optimal compromise between the design objectives. The performance of the proposed optimized model is benchmarked with one of the previously reported architectures for a similar system. The optimized model outperformed the previous model architecture with up to 55% performance improvement Apart from the effectiveness of the optimized model, the proposed design algorithm is expected to facilitate timely development of the nonparametric model of the helicopter system.
机译:在各种新兴民用应用中设计,分析和实施无人直升机系统(UHS)的高保真模型的需求不可低估。然而,采用基于控制系统动力学的物理定律的第一原理方法,由于直升机系统的复杂非线性特性,该任务被认为具有很高的挑战性。另一方面,确定用于最佳/次优性能的网络体系结构的问题一直是使用基于带有外源输入网络(NARX-network)的非线性自回归的非参数方法的主要挑战之一。 NARX网络在复杂性和准确性方面的性能在很大程度上取决于网络体系结构。文献中的当前方法主要基于反复试验,而大多数已报道的优化方法都将问题的范围限制在单个目标问题上。这项研究提出了一种用于NARX网络的常规反向传播训练算法和多目标差分进化(MODE)算法的混合,用于从实验飞行数据中识别无人小型直升机的非线性模型。所提出的混合算法能够产生在设计目标之间具有帕累托最优折衷的模型。所建议的优化模型的性能以以前报告的类似系统的体系结构之一为基准。优化后的模型在性能上比以前的模型体系结构提高了55%,除了优化后的模型的有效性外,所提出的设计算法还有望促进直升机系统非参数模型的及时开发。

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