基于ANFIS的进近阶段飞行员操纵模型设计
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  • 英文篇名:Design of Pilot Control Model in Approach Phase Based on ANFIS
  • 作者:毛忠明 ; 顾宏斌 ; 吴东苏
  • 英文作者:MAO Zhong-ming;GU Hong-bin;WU Dong-su;College of Civil Aviation, Nanjing University of Aeronautics and Astronautics;
  • 关键词:飞行员操纵模型 ; ANFIS ; 飞行员在环实验 ; 进近过程
  • 英文关键词:pilot control model;;ANFIS;;pilot-in-the-loop experiment;;approach stage
  • 中文刊名:SZJT
  • 英文刊名:Digital Technology & Application
  • 机构:南京航空航天大学民航学院;
  • 出版日期:2019-01-25
  • 出版单位:数字技术与应用
  • 年:2019
  • 期:v.37;No.343
  • 语种:中文;
  • 页:SZJT201901088
  • 页数:4
  • CN:01
  • ISSN:12-1369/TN
  • 分类号:178-181
摘要
自适应神经模糊系统(ANFIS)中的模糊推理部分能有效地模拟飞行员在操纵时的感知、决策、执行过程,人工神经网络部分能对复杂的非线性系统进行自适应学习,因此利用ANFIS对飞行员的操纵行为进行建模是非常合适的。本文基于CESSNA 172模拟器设计了飞行员在环的人机实验,通过实验采集了进近阶段飞行员的操纵数据和飞机实时响应数据,将数据处理后作为ANFIS的输入输出训练得到飞行员在进近时的操纵模型,并对模型预测效果进行了验证。ANFIS训练得到的操纵模型既可以作为进一步研究飞行员操纵行为的工具,也可以作为评判飞行员进近时操纵表现的标准。
        The fuzzy reasoning part of the ANFIS can effectively simulate the process of pilot's perception, decision-making and execution during operation, and the artificial neural network part can carry out adaptive learning for the complex nonlinear system. Therefore, it is very appropriate to use ANFIS to model pilot's control behavior. This paper designs the pilot's man-machine experiment in the loop based on CESSNA 172 simulator.Through the experiment, the pilot's control data and aircraft real-time response data are collected. The data are processed as input and output of ANFIS.Then, the pilot's control model is trained and the predictive effect of the model is verified. The control model trained by ANFIS can be used not only as a tool to further study pilot's control behavior, but also as a criterion to evaluate pilot's maneuvering performance when approaching.
引文
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