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基于ACP理论的微型扑翼飞行器的姿态控制
金龙; 李嘉昌; 常振强; 卢经纬; 程龙
Source Publication自动化学报
ISSN0254-4156
2023
Volume49Issue:12Pages:2532-2543
Abstract微型扑翼飞行器(Flapping wing micro aerial vehicle, FWMAV)因飞行效率高、质量轻、耗能低、机动性强等显著优点,在飞行器研究和应用中占据重要地位.目前, FWMAV姿态控制成为飞行器控制研究领域的研究热点.针对FWMAV姿态控制问题,基于平行智能理论框架提出了一种FWMAV抗扰动姿态控制器.通过建立人工系统(Artificial systems, A)、计算实验(Computational experiments, C)、平行执行(Parallel execution, P)三个过程,得到一个能够有效解决FWMAV姿态控制过程中扰动问题的控制器,并通过理论分析和数值仿真证明了该控制器的有效性.
Keyword微型扑翼飞行器 姿态控制 神经动力学 平行智能
DOI10.16383/j.aas.c210646
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Document Type期刊论文
Identifierhttp://ir.ia.ac.cn/handle/173211/55772
Collection学术期刊_自动化学报
Recommended Citation
GB/T 7714
金龙,李嘉昌,常振强,等. 基于ACP理论的微型扑翼飞行器的姿态控制[J]. 自动化学报,2023,49(12):2532-2543.
APA 金龙,李嘉昌,常振强,卢经纬,&程龙.(2023).基于ACP理论的微型扑翼飞行器的姿态控制.自动化学报,49(12),2532-2543.
MLA 金龙,et al."基于ACP理论的微型扑翼飞行器的姿态控制".自动化学报 49.12(2023):2532-2543.
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