基于递归高斯-牛顿的无人直升机动力学神经网络建模训练算法

S. S. Shamsudin, Xiaoqi Chen
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引用次数: 2

摘要

本文提出了一种基于递归高斯-牛顿的训练算法,利用神经网络建模方法对小型直升机系统进行动力学建模。重点研究了递归算法的优化网络选择问题,并结合交叉验证方法,使递归算法具有良好的泛化性能。然后将递归方法与离线Levenberg-Marquardt (LM)训练方法进行比较,评价模型预测的泛化性能和适应性。结果表明,递归高斯-牛顿方法的泛化性能略低于离线方法,但能很好地适应飞行过程中发生的动态变化。结果表明,该递归算法能够在给定的计算时间约束下以可接受的精度表示耦合直升机动力学。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Recursive Gauss-Newton based training algorithm for neural network modelling of an unmanned helicopter dynamics
This paper presents a recursive Gauss-Newton based training algorithm to model the dynamics of a small scale helicopter system using neural network modelling approach. It focuses on selection of optimized network for recursive algorithm that offers good generalization performance with the aid of the cross validation method proposed. The recursive method is then compared with off-line Levenberg-Marquardt (LM) training method to evaluate the generalization performance and adaptability of the model prediction. The results indicate that the recursive Gauss-Newton method gives slightly lower generalization performance compared to its off-line counterpart but adapts well to the dynamic changes that occur during flight. The proposed recursive algorithm was found effective in representing coupled helicopter dynamics with acceptable accuracy within the available computational timing constraint.
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