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基于PSoC架构的多旋翼飞行器LSTM-ASMC融合算法研究

杨茂林1,王池1,方明2,刘晓萌1,周明源3,朱广胜1   

  1. 1. 中国电子科技集团公司第五十八研究所,江苏 无锡  214072;2. 中国电子科技集团公司第三十二研究所,上海  201808;3.  中微亿芯有限公司,江苏 无锡  214072
  • 收稿日期:2025-09-08 修回日期:2025-11-12 出版日期:2025-11-18 发布日期:2025-11-18
  • 通讯作者: 杨茂林

Research on the LSTM-ASMC Fusion Algorithm for Multi-Rotor Aircraft Based on the PSoC Architecture

YANG Maolin1,WANG Chi1,FANG Ming2,LIU Xiaomeng1,ZHOU Mingyuan3,ZHU Guangsheng1   

  1. 1. China Electronics Technology Group Corporation No. 58 Research Institute, Wuxi 214035, China; 2. China Electronics Technology Group Corporation No. 32 Research Institute, Shanghai, 201808, China; 3.Wuxi Esiontech Co., Ltd., Wuxi, 214072, China
  • Received:2025-09-08 Revised:2025-11-12 Online:2025-11-18 Published:2025-11-18

摘要: 针对多旋翼飞行器在复杂风场环境下存在抖振和响应滞后的问题,提出一种基于PSoC硬件平台的神经网络增强型自适应滑模控制方法。该方法利用长短期记忆网络替换传统自适应滑模控制中的固定扰动上界估计模型,实现对滑模参数λρ的动态优化调节。然后基于集成NPU的PSoC异构计算架构实现了算法的高效部署。硬件加速性能测试以及仿真结果表明,PSoC硬件平台单样本处理时间仅需81.7 μs,支持12.24 kHz的高频闭环控制。仿真结果表明,相较于ASMC方法将系统俯仰/滚转角收敛时间从0.62 s缩短至0.27 s,滚转角抖振幅值由±1.66°抑制至±0.14°,最大偏移速度仅为±1.1 m/s。

关键词: 多旋翼飞行器, LSTM神经网络, 自适应滑模控制器, PSoC架构

Abstract: This paper addresses the issues of chattering and response lag in multi-rotor aircraft under complex wind field conditions by proposing a neural network-enhanced adaptive sliding mode control method based on a PSoC hardware platform. The method replaces the fixed disturbance upper-bound estimation model in traditional adaptive sliding mode control with a long short-term memory network, enabling dynamic optimization of the sliding mode parameters λ and ρ. Furthermore, an efficient deployment of the algorithm is achieved using the heterogeneous computing architecture of PSoC with an integrated NPU. Hardware acceleration performance tests demonstrate that the PSoC hardware platform requires only 81.7 μs for single-sample processing, supporting high-frequency closed-loop control at 12.24 kHz. Simulation results indicate that, compared to ASMC, the proposed method reduces the convergence time of the system´s pitch/roll angles from 0.62 s to 0.27 s, suppresses the roll angle buffeting amplitude from ±1.66° to ±0.14°, and maximum movement speed within is ±1.1 m/s.

Key words: multi-rotor aircraft, LSTM neural networks, ASMC, PSoC architecture