###
DOI:
飞控与探测:2025,8(6):37-47
本文二维码信息
码上扫一扫!
基于动态事件触发学习滑模的航天器编队构形维持控制
(1.南京航空航天大学 航天学院;2.西北工业大学 航天学院;3.上海航天控制技术研究所;4.上海市空间智能控制技术重点实验室;5.马鞍山学院)
Dynamic Event-Triggered Spacecraft Formation Configuration Maintenance Control via a Learning Sliding Mode Approach
(1.College of Astronautics, Nanjing University of Aeronautics and Astronautics;2.School of Astronautics, Northwestern Polytechnical University;3.Shanghai Aerospace Control Technology Institute;4.Shanghai Key Laboratory of Space Intelligent Control Technology;5.Maanshan College)
摘要
相似文献
参考文献
本文已被:浏览 479次   下载 152
    
中文摘要: 针对航天器编队通信受限和空间受摄下的构形维持控制问题,研究了一种基于学习切比雪夫神经网络(Chebyshev Neural Network,CNN) 和动态事件触发(Dynamic Event Triggering,DET)机制的控制方法。为了补偿空间干扰的影响,研究了一种基于迭代学习算法的学习CNN模型,与传统CNN 模型相比,该模型计算资源占用更少。然后,基于滑模控制理论和图论知识设计了一种终端滑模控制器。最后,为所提控制器设计了一种DET机制。仿真结果表明,所提出的控制方法能实现高精度的构形维持,并且有效减少编队集群间的通信频率超过92.01%,同时避免芝诺现象。
Abstract:To address the issue of spacecraft formation maintenance under communication constraints and space disturbances, this paper investigates a control method based on the learning Chebyshev Neural Network (CNN) and a Dynamic Event Trigger (DET) mechanism. To compensate for the effects of space disturbances, a learning CNN model based on an iterative learning algorithm is proposed, which requires fewer computational resources compared to traditional CNN models. Subsequently, a terminal sliding mode controller is designed based on sliding mode control theory and graph theory. Finally, a DET mechanism is designed for the proposed controller. Simulation results demonstrate that the proposed control method achieves high-precision formation maintenance, effectively reduces inter-formation communication frequency by over 92.01%, and avoids the Zeno phenomenon.
文章编号:20250604     中图分类号:V448.2; V412.4    文献标志码:A
基金项目:微小型航天器快速设计与智能集群全国重点实验室基金(MS01240109);南京航空航天大学科研与实践创新计划(xcxjh20241504)
引用文本:
李庚欢,贾庆贤,宋婷,孙秀芹.基于动态事件触发学习滑模的航天器编队构形维持控制[J].飞控与探测,2025,8(6):37-47.