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Modeling of Pilot Landing Approach Control Using Stochastic Switched Linear Regression Model

机译:基于随机切换线性回归模型的飞行员着陆进近控制模型

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摘要

Human pilot control during the landing approach is modeled using a stochastic switched model, which is a combination of the conventional linear regression model and a hidden Markov model. Using this model, the time histories of pilot control can be categorized in several states, such as pitch stabilizing mode. First, the selection of model inputs is discussed. Based on data obtained in flight simulator experiments, the pilot approach control model is constructed for several cases, with different wind conditions applying an expectation-maximization algorithm. The obtained models are analyzed with respect to the timing of state transitions and the stochastic-switched-model gam parameters. The current findings suggest that the proposed analysis method has a great potential to reveal a pilot's decision-making process.
机译:降落进近过程中的人类飞行员控制使用随机切换模型建模,该模型是常规线性回归模型和隐马尔可夫模型的组合。使用该模型,可以将先导控制的时间历史分为几种状态,例如俯仰稳定模式。首先,讨论模型输入的选择。根据在飞行模拟器实验中获得的数据,针对几种情况构建了驾驶员进近控制模型,并采用期望最大化算法,在不同的风况下。关于状态转变的时间和随机切换模型的游戏参数,分析了获得的模型。当前的发现表明,所提出的分析方法具有揭示飞行员决策过程的巨大潜力。

著录项

  • 来源
    《Journal of Aircraft》 |2010年第5期|p.1554-1558|共5页
  • 作者

    Ryota Mori; rnShinji Suzuki;

  • 作者单位

    Electronic Navigation Research Institute, Tokyo 182-0012, Japan Air Traffic Management Department, 7-42-23 Jindaiji-Higashimachi, Chofu-shi;

    rnUniversity of Tokyo, Tokyo 113-8656, Japan Department of Aeronautics and Astronautics, 7-3-1 Hongo, Bunkyo-ku;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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