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Identification of Helicopter Dynamics based on Flight Data using Nature Inspired Techniques

机译:基于自然飞行数据的直升机动力学识别   灵感的技巧

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摘要

The complexity of helicopter flight dynamics makes modeling and helicoptersystem identification a very difficult task. Most of the traditional techniquesrequire a model structure to be defined apriori and in case of helicopterdynamics, this is difficult due to its complexity and the interplay betweenvarious subsystems.To overcome this difficulty, non-parametric approaches arecommonly adopted for helicopter system identification. Artificial NeuralNetwork are a widely used class of algorithms for non-parametric systemidentification, among them, the Nonlinear Auto Regressive eXogeneous inputnetwork (NARX) model is very popular, but it also necessitates some in depthknowledge regarding the system being modeled. There have been many approachesproposed to circumvent this and yet still retain the advantageouscharacteristics. In this paper we carry out an extensive study of one suchnewly proposed approach using a modified NARX model with a two tiered,externally driven recurrent neural network architecture. This is coupled withan outer optimization routine for evolving the order of the system. Thisgeneric architecture is comprehensively explored to ascertain its usability andcritically asses its potential. Different instantiations of this architecture,based on nature inspired computational techniques (Artificial Bee Colony,Artificial Immune System and Particle Swarm Optimization) are evaluated andcritically compared in this paper. Simulations have been carried out foridentifying the longitudinally uncoupled dynamics. Results of identificationindicate a quite close correlation between the actual and the predictedresponse of the helicopter for all the models.
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。大多数传统技术都需要先定义模型结构,并且在直升机动力学的情况下,由于其复杂性以及各个子系统之间的相互作用,很难做到这一点。为克服这一困难,非参数方法通常用于直升机系统识别。人工神经网络是用于非参数系统识别的一种广泛使用的算法,其中,非线性自回归异质输入网络(NARX)模型非常流行,但它也需要一些关于建模系统的深度知识。已经提出了许多方法来规避这一点,但是仍然保留了有利的特性。在本文中,我们使用经过改进的NARX模型和两层外部驱动的递归神经网络体系结构,对这种新提出的方法进行了广泛的研究。这与用于优化系统顺序的外部优化例程结合在一起。对该通用体系结构进行了全面探索,以确定其可用性并严格评估其潜力。本文基于自然启发的计算技术(人工蜂群,人工免疫系统和粒子群优化)对该架构的不同实例进行了评估,并对其进行了批判性比较。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,对于所有模型,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。

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