飞翼布局飞行器研究现状分析
作者:
作者单位:

(国防科技大学 空天科学学院, 湖南 长沙 410073)

作者简介:

陈清阳(1982—),男,福建漳州人,副研究员,博士,硕士生导师,Email:chy1982_008@nudt.edu.cn

通讯作者:

中图分类号:

V279

基金项目:

国家自然科学基金资助项目


Analysis of the current research on the flying-wing aircraft
Author:
Affiliation:

(College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China)

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    对飞翼布局飞行器的发展脉络进行了梳理,涵盖了从其早期的进化史到现阶段的研究进展,并对未来的发展方向进行了思考和展望。同时,论述了飞翼布局飞行器的几个主要控制难点,具体包括:宽速域非线性状态下的姿态控制问题、多效应耦合下的高精度自主起降控制问题、气动模型近似及强扰动状态下的鲁棒控制难题,以及因多舵面冗余而引起的控制分配问题。此外,还深入讨论了当前重点研究的飞翼布局飞行器的流动控制问题,并对接下来主动流动控制技术的研究动向进行了阐述。

    Abstract:

    The development trajectory of the flying-wing aircraft was sorted out, encompassing the early evolutionary history to the current state of research, along with contemplation and forecasts regarding future directions. Meanwhile, several key control challenges associated with flying-wing aircraft were discussed, including attitude control in a wide-speed domain under nonlinear conditions, high-precision autonomous take off and landing control under multiple effect coupling, robust control issues with approximate aerodynamic models and under strong disturbances, as well as control allocation problems arising from multi-surface redundancy. Moreover, the discussion on flow control issues that were currently a focal point in flying-wing aircraft research were discussed in depth. The following research trend of active flow control technology was expounded.

    参考文献
    相似文献
    引证文献
引用本文

陈清阳,辛宏博,王鹏,等.飞翼布局飞行器研究现状分析. Analysis of the current research on the flying-wing aircraft[J].国防科技大学学报,2024,46(3):39-58.

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2022-03-01
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2024-06-18
  • 出版日期: 2024-06-28
文章二维码