Pilot-in-the-Loop Analysis of Aileron Operation and Flight Simulator Experiments

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Lateral-directional piloted simulation experiments were conducted in order to analyze pilot responses when the pilot controls an aircraft with only the ailerons after rudder failure. The experiments were carried out using a fixed-base flight simulator and four pilots. Six aircraft configurations, made by changing the stability derivatives, were tested, and pilot models were identified using the least-squares method. An analysis of the closed-loop shows that the closed-loop gain and stabilities correlate with the tracking error of the compensation task. Additionally, from the results of analysis, an evaluation function using pilot-in-the-loop with a fixed pilot model was developed. This function was able to predict the compensational error analytically from the airplane dynamics.

収録刊行物

  • Transactions of the Japan Society for Aeronautical and Space Sciences  

    Transactions of the Japan Society for Aeronautical and Space Sciences 50(169), 193-200, 2007-11-04 

    THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

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各種コード

  • NII論文ID(NAID)
    10021152373
  • NII書誌ID(NCID)
    AA0086707X
  • 本文言語コード
    ENG
  • 資料種別
    ART
  • ISSN
    05493811
  • NDL 記事登録ID
    9254569
  • NDL 雑誌分類
    ZN25(科学技術--運輸工学--航空機・ロケット)
  • NDL 請求記号
    Z53-M236
  • データ提供元
    CJP書誌  NDL  J-STAGE 
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