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Modeling and Control for A Non-Linear Dynamical Hypersonic Aircraft

机译:非线性动力高超音速飞机的建模与控制

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摘要

According to the Lagrange's Equations,a non-linear dynamics modeling for hypersonic aircrafts like X-43 is proposed in this paper.The nonlinear physics-based models of the longitudinal and lateral dynamics for X-43 are developed.At the same time,a simulation for the longitudinal model of X-43 is given.The analysis and the derivation process of the model provide tools for further researchers who face the control problems of hypersonic aircraft X-43.
机译:根据拉格朗日方程,本文提出了一种用于X-43等高超音速飞机的非线性动力学模型。建立了基于非线性物理学的X-43纵向和横向动力学模型。对X-43纵向模型进行了仿真分析。模型的分析和推导过程为面临高超声速飞机X-43控制问题的进一步研究人员提供了工具。

著录项

  • 来源
  • 会议地点 Dali(CN);Dali(CN)
  • 作者

    CHI Yu-lian;

  • 作者单位

    Yinxing Hao@Laboratory of Complex Systems and Intelligence Science,Institute of Automation,Chinese Academy of Sciences,Beijing,P.R.China,100080--Jianqiang Yi@Laboratory of Complex Systems and Intelligence Science,Institute of Automation,Chinese Academy of Sciences,Beijing,P.R.China,100080--Dongbin Zhao@Laboratory of Complex Systems and Intelligence Science,Institute of Automation,Chinese Academy of Sciences,Beijing,P.R.China,100080--Xiangmin Tan@Laboratory of Complex Systems and Intelligence Science,Institute of Automation,Chinese Academy of Sciences,Beijing,P.R.China,100080--;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 人工智能理论;
  • 关键词

    Hypersonic aircraft; Dynamics model; Modeling; Control;

    机译:高超音速飞机;动力学模型;建模;控制;

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