首页 >

基于激光雷达实测风场的前馈阵风载荷控制

戴玉婷1,胡雅婷1,杨超1,陈同银2   

  1. 1. 北京航空航天大学
    2. 沈阳飞机设计研究所
  • 收稿日期:2026-02-09 修回日期:2026-05-27 出版日期:2026-05-28 发布日期:2026-05-28
  • 通讯作者: 戴玉婷
  • 基金资助:
    国家自然科学基金;国家自然科学基金

Feedforward Gust Load Alleviation Control Based on Lidar-Measured Wind Fields

  • Received:2026-02-09 Revised:2026-05-27 Online:2026-05-28 Published:2026-05-28
  • Contact: Dai Yu-Ting

摘要: 前馈阵风载荷控制根据探测的阵风风场与先验知识,驱动舵面偏转以抑制阵风响应。开发了基于激光雷达的多点风速测量方法与飞机运动下的风速解算方法,能测量运动飞机的前方30到70米处不同位置的垂直风速与水平风速。对激光测风雷达进行地面静、动平台下的风速测量试验,验证了机载激光雷达风速测量的正确性。在此基础上,在楼房10楼顶层平台采用激光测风雷达连续3天测量前方30-70米的开阔地带自然风速,发现如下规律:水平风速随时间连续、随空间过渡均匀,而垂向风速在空间、时间尺度上变化明显,不同的时空风速使用策略表明,采用较高的时间采样率能够得到更准确的风场。基于激光雷达实测的风速,发展CFD环境的弹性机翼流固耦合仿真[1]与先验知识驱动的前馈阵风载荷控制。四种实测阵风工况下,前馈阵风载荷控制的均方根、峰值减缓率在58.4 ~ 85.5%,对于风速脉动剧烈或峰值大的阵风工况,前馈控制均能产生较好的阵风减缓效果。与前馈控制相比,反馈控制在风速迅速变化时难以及时控制或超调。

关键词: 阵风减缓, 激光测风雷达, 前馈控制, 流固耦合, 阵风载荷

Abstract: Feedforward gust load control (GLC) suppresses gust responses by driving control surface deflections based on detected gust wind fields and prior knowledge. In this study, a LiDAR-based multi-point wind speed measurement method and a wind speed calculation algorithm considering aircraft motion were developed, enabling the measurement of vertical and horizontal wind speeds at various positions 30-70 meters ahead of a moving aircraft. Ground-based experiments on both static and dynamic platforms were conducted to verify the accuracy of the airborne LiDAR wind measurement system. Subsequently, a three-day continuous measurement of natural wind speeds over an open area (30-70m range) was performed using the LiDAR from a 10th-floor rooftop platform. The results indicate that while horizontal wind speed is continuous in time and transitions uniformly in space, vertical wind speed exhibits significant variations across both spatial and temporal scales. Evaluations of different spatiotemporal sampling strategies suggest that a higher temporal sampling rate yields a more accurate representation of the wind field. Based on the LiDAR-measured wind speeds, a fluid-structure interaction simulation for elastic wings was developed within a CFD environment, integrated with prior knowledge-driven feedforward GLC. Under four measured gust conditions, the feedforward GLC achieved reduction rates of 58.4% to 85.5% in terms of root mean square and peak values. For gust conditions characterized by intense fluctuations or high peak velocities, the feedforward control demonstrated robust mitigation effects. In contrast, feedback control struggled with latency or overshoot during rapid wind speed transitions.

Key words: Gust Alleviation, Lidar Wind Measurement, Feedforward Control, Fluid-Structure Interaction, Gust Load

中图分类号: