使用基于 BSO 算法的 ANFIS 模型改进无人飞行器的推力

M. Konar, S. ARIK HATİPOĞLU, M. Akpınar
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引用次数: 0

摘要

无人驾驶飞行器(UAV)如今已在我们生活的许多领域出现,随着技术的不断发展,它们也带来了新的期望和需求。为了满足这些期望和需求,无人飞行器设计必须考虑降低能耗、增加推力和续航时间等主要问题。本研究首次提出了基于回溯搜索优化(BSO)算法的自适应神经模糊推理系统(ANFIS)模型,以提高无人机的推力。为此,首先在推力测量装置上测试了不同的电池和螺旋桨,并获得了一组数据。螺旋桨直径和螺距、电流、电压和电子速度控制器(ESC)信号被选为输入,无人机推力被选为输出。ANFIS 用于将输入和输出参数之间没有直接关系的参数联系起来。为了确定 ANFIS 参数的最佳值,使用 BSO 算法对获得的数据集进行 ANFIS 训练。然后,将基于最佳 ANFIS 结构的目标函数集成到 BSO 算法中,并使用 BSO 算法计算出能产生最佳推力的输入值。仿真结果同样考虑了影响推力的发动机、电池和螺旋桨等参数,表明所提出的方法可有效改善无人机的推力。这种由 ANFIS 和 BSO 算法组成的混合方法可以减少无人机设计中的成本和时间损失,并允许对多种可能性进行测试。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Improvement of UAV thrust using the BSO algorithm-based ANFIS model
Unmanned aerial vehicles (UAVs), which are available in our lives in many areas today, bring with them new expectations and needs along with developing technology. In order to meet these expectations and needs, main subjects such as reducing energy consumption, increasing thrust and endurance, must be taken into account in UAV designs. In this study, Backtracking search optimisation (BSO) algorithm-based adaptive neuro-fuzzy inference system (ANFIS) model is proposed for the first time to improve UAV thrust. For this purpose, first, different batteries and propellers were tested on the thrust measuring device and a data set was obtained. Propeller diameter and pitch, current, voltage and the electronic speed controller (ESC) signal were selected as input, and UAV thrust was selected as output. ANFIS was used to relate input and output parameters that do not have a direct relationship between them. In order to determine the ANFIS parameters at the optimum value, ANFIS was trained with the obtained data set by using BSO algorithm. Then, the objective function based on the optimum ANFIS structure was integrated into BSO algorithm, and the input values that gave the optimum thrust were calculated using BSO algorithm. Simulation results, in which parameters such as engine, battery and propeller affecting the thrust are taken into account equally, emphasise that the proposed method can be used effectively in improving the UAV thrust. This hybrid method, consisting of ANFIS and BSO algorithm, can reduce the cost and time loss in UAV designs and allows many possibilities to be tested.
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