混合饥饿游戏搜索优化的神经网络方法应用于无人机

IF 3.2 Q3 Mathematics
Nadia Samantha Zuñiga-Peña , Salatiel Garcia-Nava , Norberto Hernandez-Romero , Juan Carlos Seck-Touh-Mora
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引用次数: 0

摘要

优化方法,如基于群体的算法,在应用于多维和非线性问题时是有价值的。许多工程问题,如控制器参数化,可以使用基于种群的算法来解决,因为这些参数通常是通过论文找到的,这会导致大量的时间和资源消耗。基于种群的算法需要定义搜索最佳解决方案的范围,即搜索空间。然而,由于应用这些控制器的系统的非线性性质,必须定义的搜索空间是不确定的。本文提出了一种将饥饿游戏搜索(HGS)元启发式算法与无监督自组织地图Kohonen神经网络相结合的混合优化策略,以改善无人驾驶飞行器(uav)运输缆索悬吊载荷的轨迹跟踪控制。在提出的NNHGS中,HGS算法寻求最小化均方根跟踪误差(RMSE)的控制器增益。同时,神经网络根据不断变化的跟踪性能不断重塑搜索区间。通过将探索扩展到初始边界以外的参数区域,NNHGS找到了标准HGS排除的高质量解。采用超扭滑模控制器(STSMC)的仿真结果表明,NNHGS将最终跟踪误差从HGS的RMSE=0.0480减小到NNHGS的RMSE= 0.0204,并且具有增强的抗干扰能力和对参数变化的快速适应能力。这些成果突出了这种方法在现实任务中的适用性,如后勤、救灾或远程检查,在这些任务中,无人机必须在不确定或参数变化的条件下保持稳定。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Hybrid Hunger Games Search optimization using a neural networks approach applied to UAVs
Optimization methods like population-based algorithms are valuable when applied to multidimensional and nonlinear problems. Many engineering problems, such as controller parameterization, can be addressed using population-based algorithms since these parameters are usually found through essays, resulting in high time and resource consumption. Population-based algorithms need to define the range within which the search for the best solution is performed, known as the search space. However, due to the nonlinear nature of the systems to which these controllers are applied, there is no certainty about the search space that must be defined. This study proposes a hybrid optimization strategy that couples the Hunger Games Search (HGS) metaheuristic with an unsupervised Self Organizing Map, Kohonen Neural Network, to improve trajectory-tracking control of unmanned aerial vehicles (UAVs) transporting cable suspended loads. In the proposed NNHGS, the HGS algorithm seeks the controller gains that minimize Root Mean Square tracking Error (RMSE). At the same time, the neural network continuously reshapes the search intervals according to the evolving tracking performance. By expanding the exploration into parameter regions beyond the initial bounds, the NNHGS finds high-quality solutions that standard HGS excludes. The simulation results obtained with a Super Twisting Sliding Mode Controller (STSMC) show a reduction in the final tracking error from RMSE=0.0480 with HGS to RMSE = 0.0204 by NNHGS, along with enhanced disturbance rejection and rapid adaptation to parameter changes. These gains highlight the suitability of this method for real-world missions such as logistics, disaster relief, or remote inspection, where UAVs must remain stable under uncertain or parameter-varying conditions.
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来源期刊
Results in Control and Optimization
Results in Control and Optimization Mathematics-Control and Optimization
CiteScore
3.00
自引率
0.00%
发文量
51
审稿时长
91 days
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