Modeling of unmanned small scale rotorcraft based on Neural Network identification

I. E. Putro, A. Budiyono, K. Yoon, D. H. Kim
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引用次数: 24

Abstract

Design and development of Unmanned Aerial Vehicles has attracted increased interest in the recent past. Rotorcraft UAVs, in particular have more challenges than its fixed wing counterparts. More research and experiments have been conducted to study the stability and control of RUAVs. A model-based control system design is particularly of our interest since it avoids a tedious trial and error process. To be able to successfully stabilize and control the RUAVs therefore a sufficiently accurate model is necessary. There are many methods in modeling small-scale rotorcraft. Using a standard first-principle based modeling approach, considerable knowledge about rotorcraft flight dynamics is required to derive the governing equation. Another method is system identification from flight data. This paper presents a method for system identification using Neural Networks. Input-output data are provided from nonlinear simulation of X-Cell 60 small scale helicopter. The data is used to train the multi-layer perceptron combined with NNARXM time regression input vector to learn nonlinear behavior of the vehicle.
基于神经网络辨识的小型无人旋翼机建模
近年来,无人驾驶飞行器的设计和发展引起了越来越多的兴趣。特别是旋翼无人机比固定翼无人机面临更多挑战。对无人机的稳定性和控制进行了更多的研究和实验。基于模型的控制系统设计是我们特别感兴趣的,因为它避免了繁琐的试错过程。为了能够成功地稳定和控制ruav,因此一个足够精确的模型是必要的。小型旋翼机的建模方法有很多。使用标准的基于第一性原理的建模方法,需要大量关于旋翼飞机飞行动力学的知识来推导控制方程。另一种方法是根据飞行数据进行系统识别。本文提出了一种利用神经网络进行系统辨识的方法。通过对小型直升机X-Cell 60的非线性仿真,给出了输入输出数据。该数据用于训练结合NNARXM时间回归输入向量的多层感知器,以学习车辆的非线性行为。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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