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带有升降气囊与压块的飞艇动力学建模

蔡自立 屈卫东 席裕庚

蔡自立, 屈卫东, 席裕庚. 带有升降气囊与压块的飞艇动力学建模[J]. 应用数学和力学, 2005, 26(8): 979-987.
引用本文: 蔡自立, 屈卫东, 席裕庚. 带有升降气囊与压块的飞艇动力学建模[J]. 应用数学和力学, 2005, 26(8): 979-987.
CAI Zi-li, QU Wei-dong, XI Yu-geng. Dynamic Modeling for Airship Equipped With Ballonets and Ballast[J]. Applied Mathematics and Mechanics, 2005, 26(8): 979-987.
Citation: CAI Zi-li, QU Wei-dong, XI Yu-geng. Dynamic Modeling for Airship Equipped With Ballonets and Ballast[J]. Applied Mathematics and Mechanics, 2005, 26(8): 979-987.

带有升降气囊与压块的飞艇动力学建模

基金项目: 国防重大预研项目(415011102)
详细信息
    作者简介:

    蔡自立(1974- ),男,湖北人,博士(联系人.Tel/Fax:+86-21-62932005;E-mail:zili-cai@126.com).

  • 中图分类号: N945.12

Dynamic Modeling for Airship Equipped With Ballonets and Ballast

  • 摘要: 研究飞艇的动力学建模,将飞艇的机体视为浮力与重力相等的浸没刚体,且考虑了飞艇机体与升降气囊以及压块之间的动力学耦合作用.整体的动力学方程首先通过Newton-Euler定律和Kirchhoff方程推出.此外,应用Hamilton与Lagrange半直积约化理论,可以将动力学方程解释为Lie-Poisson系统或者Euler-Poincaré系统.这两种动力学描述在基于能量的控制设计中有着重要作用.
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    [7] Ortega R,Spong Mark W,Gómez-Estern F,et al.Stabilization of a class of underactuated mechanical systems via interconnection and damping assignment[J].IEEE Transaction on Automatic Control,2002,47(12):1218—1233. doi: 10.1109/TAC.2002.800770
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  • 被引次数: 0
出版历程
  • 收稿日期:  2003-10-14
  • 修回日期:  2005-03-10
  • 刊出日期:  2005-08-15

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