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一种基于NARX神经网络的纵向飞行动力学建模方法

A longitudinal flight dynamics modeling method based on NARX neural network
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摘要 针对传统飞行动力学建模工作量大、周期长等问题,提出了一种基于飞行包线离散化和数据驱动的纵向飞行动力学建模方法。以F-16为例,首先分析了纵向运动模态,开展了纵向单脉冲模拟试飞生成特征样本集;然后,利用模糊c-均值算法对样本集进行聚类,选择并设计了综合有效性指标以确定最优聚类数,实现了飞行包线离散化;最后,在子包线内选用训练样本集对NARX神经网络进行训练以建立纵向飞行动力学模型,使用同一子包线内的验证样本集验证模型。结果表明,子包线实现了全覆盖且相邻包线之间边界清晰无重叠,模型输出结果平均相对误差均在3%以内,说明该方法对开展飞机纵向飞行动力学建模是可行的和有效的,为纵向飞行动力学建模提供了一种新思路。 Aiming at the large workload and long period of traditional flight dynamics modeling,a longitudinal flight dynamics modeling method based on flight envelope discretization and data-driven is proposed.Taking the F-16 as an example,the longitudinal motion mode was firstly analyzed,and the longitudinal single-pulse simulation flight test was carried out to generate characteristic sample sets.Then,used the fuzzy c-means algorithm to cluster the sample sets,selected and designed the comprehensive cluster validity to determine the optimal number of clusters,and realized the discreti-zation of the flight envelope.Finally,the training sample set was selected in the sub-envelope to train the NARX neural network so as to establish the longitudinal flight dynamics model,and the validation sample set in the same sub-envelope was used to validate the model.The results show that the sub-envelopes achieve the full coverage and the boundaries between adjacent envelopes are clear and non-overlapping.The average relative error of the model output results is within 3%.It shows that the method is feasible and effective for the modeling of aircraft longitudinal flight dynamics.Also,it provides a new idea for longitudinal flight dynamics modeling.
作者 陈开民 顾宏斌 李鹏 范志鹏 魏小峰 CHEN Kaimin;GU Hongbin;LI Peng;FAN Zhipeng;WEI Xiaofeng(Center for Flight Simulation and Advanced Technology for Training,NUAA,Nanjing 210016,China;College of Automobile and Traffic Engineering,NFU,Nanjing 210037,China;Flight Test Center,COMAC,Shanghai 200232,China;China Simulation Sciences Co.,Ltd.,Shanghai 201315,China)
出处 《飞行力学》 CSCD 北大核心 2023年第5期37-43,51,共8页 Flight Dynamics
基金 上海市浦江人才计划资助(22PJ1420900)。
关键词 飞行动力学 数据驱动 模糊C-均值 NARX神经网络 flight dynamics data-driven fuzzy c-means NARX neural network
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  • 1杨莉,汪叔华.采用BP神经网络的惯导初始对准系统[J].南京航空航天大学学报,1996,28(4):487-491. 被引量:29
  • 2夏恩松,王艳东.直接对准算法及遗传算法在SINS初始对准中的应用研究[J].宇航学报,2006,27(5):1091-1095. 被引量:4
  • 3谷宏强,袁亚雄,李斌.遗传算法在捷联惯导系统初始对准中的应用研究[J].兵工学报,2007,28(6):677-681. 被引量:3
  • 4National Research Council. Aviation safety and control: understanding and preventing unfavorable pilot-vehicle in- teractions [ M ]. Washington, D C: National Academy Press, 1997 : 14-15.
  • 5Klyde D H. Unified pilot-induced oscillation theory Vol- ume I : PIO analysis with linear and nonlinear effective ve- hicle characteristics, including rate limiting [ R ]. Califor- nia, USA : System Technology, Inc, 1995 : 14-29.
  • 6Dr Anderson M R. Unified pilot-induced oscillation theory Volume III: PIO analysis using multivariable methods [ R ]. Virginia : Department of Aerospace and Ocean Engi- neering Virginia Polytechnic Institute and State Universi- ty, 1995 : 11-46.
  • 7Jeram G J, Prasad J V R. Fuzzy logic detector for pilot in- duced oscillation [ C ]//Proceedings of the American Hel- icopter Society 59th Annual Forum. Phoenix, Arizona, USA, 2003 : 24-27.
  • 8Tian Fu-li, YU Zhi-gang, GAO Zheng-hong. Application of Gaussian complex wavelet in APC identification [ C ]//5 th International Congress of the Aeronautical Sciences. Ham- burg, Germany ,2006 : 155-158.
  • 9丁玉美 高西全.数字信号处理[M].西安:西安电子科技大学出版社,2002..
  • 10王希彬,赵国荣,高青伟.BP神经网络在惯导系统传递对准中的应用[J].海军航空工程学院学报,2008,23(5):489-492. 被引量:3

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