基于数据驱动风场估计的大气参数重构算法研究
DOI:
CSTR:
作者:
作者单位:

南京航空航天大学自动化学院导航研究中心 南京 211106

作者简介:

通讯作者:

中图分类号:

TN06;V241

基金项目:


Research on air parameter reconstruction algorithms based on data-driven wind field estimation
Author:
Affiliation:

Navigation Research Center, College of Automation, Nanjing University of Aeronautics and Astronautics,Nanjing 211106, 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:

    针对飞行器在跨音速、大机动等复杂飞行状态下因气流分离与激波干扰导致大气数据系统(ADS)测量精度下降的问题,提出了一种基于数据驱动风场估计,结合速度矢量三角形解算的大气参数重构方法。所提方法基于历史飞行数据,采用最小二乘多项式拟合算法对风速进行预测,并利用速度矢量三角形模型反向解算真空速,进而重构迎角(AOA)、侧滑角(AOS)与马赫数等关键大气参数。仿真结果表明,所提方法在复杂环境的大气参数重构中精度显著提升:原始测量迎角波动约为2°,侧滑角波动约为1°,以平均绝对值误差(MAE)和均方根误差(RMSE)为评价标准,所提方法计算迎角误差为0.47°、0.50°,侧滑角误差为0.20°、0.24°,马赫数误差为0.005 5、0.006 3。此外,研究还对比了基于冻结风场理论的估计方法,二者均能有效降低迎角与侧滑角测量误差。本研究为复杂飞行环境下高精度、高可靠性的大气数据测量提供了一种不依赖额外硬件的软件解决方案。

    Abstract:

    Aiming at the problem of degraded measurement accuracy in air data systems (ADS) caused by airflow separation and shock wave interference during complex flight conditions such as transonic regimes and high maneuverability, this paper proposes an atmospheric parameter reconstruction method based on datadriven wind field estimation combined with velocity vector triangle resolution. Utilizing historical flight data, the method employs a least squares polynomial fitting algorithm for wind speed prediction and leverages a velocity vector triangle model to inversely compute true airspeed, thereby reconstructing key atmospheric parameters including angle of attack (AOA), angle of sideslip (AOS), and Mach number. Simulation results demonstrate that the proposed method achieves significant accuracy improvement in atmospheric parameter reconstruction under complex conditions: The original AOA measurements fluctuate around 2°, while the original AOS measurements fluctuate around 1°. Evaluated using mean absolute error (MAE) and root mean squared error (RMSE) metrics, the errors are 0.47° (MAE) and 0.50° (RMSE) for AOA, 0.20° (MAE) and 0.24° (RMSE) for AOS, 0.005 5 (MAE) and 0.006 3 (RMSE) for Mach number. Additionally, the study compares the proposed method with an atmospheric parameter estimation approach based on the frozen wind field theory, with both methods effectively reducing measurement errors in AOA and AOS. This research provides a software solution for high-precision, highly reliable air data measurement in complex flight environments without requiring additional hardware.

    参考文献
    相似文献
    引证文献
引用本文

夏兆祥,李荣冰,程鉴皓,宋浩.基于数据驱动风场估计的大气参数重构算法研究[J].电子测量技术,2026,49(11):118-128

复制
分享
相关视频

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:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2026-09-03
  • 出版日期:
文章二维码

重要通知公告

①《电子测量技术》期刊收款账户变更公告