刘双源,贾心怡,王早,等. 基于改进麻雀搜索算法的无人机姿态跟踪PID参数整定[J]. 南昌航空大学学报(自然科学版),2026,40(4):38-47. doi: 10.3969/j.issn.2096-8566.2026.04.005
引用本文: 刘双源,贾心怡,王早,等. 基于改进麻雀搜索算法的无人机姿态跟踪PID参数整定[J]. 南昌航空大学学报(自然科学版),2026,40(4):38-47. doi: 10.3969/j.issn.2096-8566.2026.04.005
Liu Shuangyuan,Jia Xinyi,Wang Zao,et al. PID parameter tuning of UAV attitude tracking based on improved sparrow search algorithm[J]. Journal of Nanchang Hangkong University (Natural Sciences),2026,40(4):38-47. doi: 10.3969/j.issn.2096-8566.2026.04.005
Citation: Liu Shuangyuan,Jia Xinyi,Wang Zao,et al. PID parameter tuning of UAV attitude tracking based on improved sparrow search algorithm[J]. Journal of Nanchang Hangkong University (Natural Sciences),2026,40(4):38-47. doi: 10.3969/j.issn.2096-8566.2026.04.005

基于改进麻雀搜索算法的无人机姿态跟踪PID参数整定

PID Parameter Tuning of UAV Attitude Tracking Based on Improved Sparrow Search Algorithm

  • 摘要: 参数整定是PID控制器设计中的关键环节,传统依赖人工经验的方法耗时耗力,应用于无人机姿态跟踪控制时易局部收敛。为此,引入优化算法实现参数自动整定具有重要意义。本文提出一种改进麻雀搜索算法(ISSA),以降低麻雀搜索算法(SSA)陷入局部最优的可能性,提升全局寻优能力,从而有效解决参数整定过程中效率低、依赖人工的问题。ISSA首先通过混合扰动策略初始化种群,增强全局探索能力;其次,在发现者阶段引入自适应权重、柯西扰动和Lévy飞行机制,提高搜索灵活性与适应性;最后,在跟踪阶段采用动态香味策略,以提高局部搜索精度与收敛速度。通过无人机姿态跟踪控制的参数整定实验,验证了该算法的可行性与实用价值。

     

    Abstract: Parameter tuning is a critical step in PID controller design. The traditional method relying on manual experience is time-consuming and labor-intensive, and it is prone to falling into local optima when applied to UAV attitude tracking control. Therefore, it is of great significance to introduce optimization algorithms for automatic parameter tuning. This paper proposes an improved sparrow search algorithm (ISSA) to reduce the possibility of the original sparrow search algorithm (SSA) falling into local optima, enhance the global ooptimization capability, and thus effectively solve the problems of low efficiency and manual dependence in the tuning process. In ISSA, firstly, a hybrid perturbation strategy is used to initialize the population, strengthening global exploration ability. Secondly, adaptive weights, Cauchy perturbation, and Lévy flight are introduced into the discoverer phase to improve search flexibility and adaptability. Finally, a dynamic scent strategy is adopted in the tracking phase to enhance local search accuracy and convergence speed. The feasibility and practical value of the proposed algorithm are validated through parameter tuning experiments for UAV attitude tracking control.

     

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