Non-linear system identification of the dynamics of aeroelastic instability suppression based on targeted energy transfers

著录项

• 来源
  《Aeronautical journal》 |2010年第1152期|p.61-82|共22页
• 作者

  Y. S. Lee; A. F. Vakakis; D. M. McFarland; L. A. Bergman;

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• 作者单位

  Department of Mechanical and Aerospace Engineering New Mexico State University, Las Cruces USA;

  Department of Mechanical Science and Engineering, University of Illinois at Urbana-Champaign Urbana, Illinois USA;

  Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana USA;

  Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana USA;

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• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  H·: Hilbert transform; x_k~((m)): the m~(th) component of the k~(th) measurement in IMOs; y,α,v,(v,): heave, pitch, and NES (NES1) modes, respectively; y_k~((m))(C_m~((k))): the m~(th) component of the k~(th) measurement for an analytical (empirical) model; θ_k~((m)): instantaneous slow phase of an IMF c_m~((k)); et al;

  机译：H [·]：希尔伯特变换;x_k〜（（m））：IMO中第k〜（th）个测量的第m〜th个分量;y;α;v;（v;）：分别为升沉;俯仰和NES（NES1）模式;y_k〜（（m））（C_m〜（（k）））：分析模型（经验模型）的第k个测量值的第m个分量;θ_k〜（（m））：IMF的瞬时慢相位c_m〜（（k））;等;