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Longitudinal Automatic Landing Control for Carrier-Based Aircraft Under Complex Sea Conditions
编号：11 访问权限：仅限参会人 更新：2025-04-09 16:27:08 浏览：16次 口头报告

报告开始：暂无开始时间（Asia/Shanghai）

报告时间：暂无持续时间

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摘要
Facing the difficult problem of carrier-based aircraft landing in multi-scenarios and a complex environment, a longitudinal automatic landing control method for carrier-based aircraft based on incremental nonlinear dynamic inverse and L1 nonlinear guidance law is proposed. A carrier-based aircraft dynamics model, a ground effect model, a ship wake turbulence model and a deck motion model are established, L1 nonlinear guidance law is designed to generate longitudinal acceleration commands, pitch angle commands are derived through gravity compensation, and the attitude loop is designed to generate angular velocity commands by using the nonlinear dynamic inverse control method, which is inputted into the incremental dynamic inverse-based angular acceleration controller. The simulation results show that the designed automatic landing control method can mitigate the interference from complex sea states and improve the robustness and safety of the landing.
关键词
carrier-based aircraft landing,L1 nonlinear guidance,ship wake turbulence,deck motion
报告人
Xiaomin Zhang
Student Northwestern Polytechnical University

稿件作者
Xiaomin Zhang Northwestern Polytechnical University
Ban Wang Northwestern Polytechnical University
Lingxia Mu Xi’an University of Technology
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重要日期

  • 会议日期

    08月22日

    2025

    至

    08月24日

    2025

  • 04月25日 2025

    初稿截稿日期

主办单位
中国自动化学会技术过程的故障诊断与安全性专业委员会
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新疆大学
新疆自动化学会
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