光学助降系统引导下舰载机着舰人机系统建模
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  • 英文篇名:Modeling of man-aircraft system for carrier landing with FLOLS
  • 作者:陈晨 ; 屈香菊
  • 英文作者:CHEN Chen;QU Xiang-ju;School of Aeronautic Science and Engineering,BUAA;
  • 关键词:菲涅耳光学助降系统 ; 着舰 ; 人机系统 ; 感知模型 ; 模糊控制理论
  • 英文关键词:FLOLS;;carrier landing;;man-aircraft system;;sensing model;;fuzzy control theory
  • 中文刊名:FHLX
  • 英文刊名:Flight Dynamics
  • 机构:北京航空航天大学航空科学与工程学院;
  • 出版日期:2018-05-02 10:30
  • 出版单位:飞行力学
  • 年:2018
  • 期:v.36;No.162
  • 基金:国家自然科学基金资助(11502008)
  • 语种:中文;
  • 页:FHLX201804003
  • 页数:5
  • CN:04
  • ISSN:61-1172/V
  • 分类号:14-18
摘要
针对菲涅耳光学助降系统(Fresnel lens optical landing system,FLOLS)引导和甲板指挥官(landing signal officer,LSO)指挥下的着舰飞行中,驾驶员对FLOLS光学引导信息感知的模糊特性,基于模糊控制理论建立了舰载机着舰过程的驾驶员感知模型。在此基础上,考虑了驾驶员、LSO和舰载机,以及来自航母、舰尾流的扰动,建立了多源引导的人机系统模型。仿真结果表明了模型的合理性。该模型不仅能用于舰载机的飞行品质和安全性分析,也可以应用于FLOLS的引导灯组设计。
        By focusing on fuzzy pilot sensing process of Fresnel lens optical landing system(FLOLS)guidance information,pilot sensing model is built based on fuzzy control theory during carrier landing flight guided by both FLOLS and landing signal officer(LSO). Based on pilot sensing model,a model of man-aircraft system for multi-guided carrier landing flight is built by considering pilot,LSO,aircraft,and disturbance of carrier and carrier air wake. The proposed man-aircraft model was validated by simulation results of carrier landing flight guided by both FLOLS and LSO,and can be applied not only in flying quality and safety analysis of carrier landing flight but also in researches about FLOLS configuration design.
引文
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