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基于副气囊耦合的飞艇纵向运动影响分析

游颖捷 糜攀攀 吕明云 刘文定

游颖捷, 糜攀攀, 吕明云, 等 . 基于副气囊耦合的飞艇纵向运动影响分析[J]. 北京航空航天大学学报, 2016, 42(6): 1303-1310. doi: 10.13700/j.bh.1001-5965.2015.0427
引用本文: 游颖捷, 糜攀攀, 吕明云, 等 . 基于副气囊耦合的飞艇纵向运动影响分析[J]. 北京航空航天大学学报, 2016, 42(6): 1303-1310. doi: 10.13700/j.bh.1001-5965.2015.0427
YOU Yingjie, MI Panpan, LYU Mingyun, et al. Airship's longitudinal motion impact analysis based on coupling ballonet[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1303-1310. doi: 10.13700/j.bh.1001-5965.2015.0427(in Chinese)
Citation: YOU Yingjie, MI Panpan, LYU Mingyun, et al. Airship's longitudinal motion impact analysis based on coupling ballonet[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1303-1310. doi: 10.13700/j.bh.1001-5965.2015.0427(in Chinese)

基于副气囊耦合的飞艇纵向运动影响分析

doi: 10.13700/j.bh.1001-5965.2015.0427
基金项目: 中航工业产学研专项(Cxy2014BH04)
详细信息
    作者简介:

    游颖捷 女,硕士研究生。主要研究方向:飞行动力学与控制仿真。Tel.:010-82338116 E-mail:15201443795@163.com;糜攀攀 男,硕士研究生。主要研究方向:飞行动力学与控制仿真。Tel.:010-82338116 E-mail:BluceMi@163.com;吕明云 男,博士,教授,博士生导师。主要研究方向:飞行器总体设计、飞行器隐身技术。Tel.:010-82338116 E-mail:lv503@buaa.edu.cn

    通讯作者:

    吕明云,Tel.:010-82338116 E-mail:lv503@buaa.edu.cn

  • 中图分类号: V274

Airship's longitudinal motion impact analysis based on coupling ballonet

  • 摘要: 高空大型飞艇副气囊体积占比很大,甚至达90%以上,副气囊动力学对飞艇运动产生较大影响。对巡航高度为6 000 m的某大型飞艇,建立基于圆柱容器的副气囊动力学模型,进一步构建考虑副气囊的飞艇纵向耦合动力学方程,并对飞艇纵向运动进行了数值仿真,将其与不考虑副气囊时的结果进行对比。结果表明:副气囊对大型飞艇俯仰运动有较大影响,容易引起运动发散,且耦合影响随飞艇高度增大而变小,同时副气囊体积不变时,其直径越小,动力学耦合效应影响越小;副气囊效应会降低飞艇的操纵性,在进行飞艇设计时应该予以考虑。

     

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出版历程
  • 收稿日期:  2015-06-25
  • 网络出版日期:  2016-06-20

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