一种飞行器自动化舱段对接系统设计与实现
DOI:
CSTR:
作者:
作者单位:

1.中国航天科工集团驻系统工程公司质量监督室;2.空装驻北京地区第二军事代表室

作者简介:

通讯作者:

中图分类号:

V19

基金项目:


Automated Vehicle Segment Docking System Based on Multimodal Data Fusion Design and Implementation
Author:
Affiliation:

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:

    对固定翼飞行器舱段传统人工对接方式效率低、精度差、依赖经验等问题进行了研究,旨在开发基于多模态数据融合的自动化舱段对接系统。通过采用视觉、测距与力传感器等多模态数据实时采集技术,结合伺服控制与AI图像处理算法,构建了包含轴线对准、径向对接与控制反馈的三阶段自动化对接流程,实现了舱段位姿的精准调整与实时监测。硬件系统设计集成了高精度传感器、可移动调节平台及综合控制板,并开发主控软件实现多模态数据融合与闭环控制。经自动化对接试验验证,系统成功完成不同形态舱段的高精度对接,对接效率显著提升,人工干预减少90%以上,降低碰撞风险,满足复杂工况下的工程应用需求。结果表明,该系统有效提升了对接一致性与可靠性,为飞行器模块化装配提供了高效解决方案,适用于不同类型和尺寸的舱段对接任务。此外,针对现有系统的局限性,提出了进一步优化多自由度调节功能的方向。

    Abstract:

    A study was conducted on the low efficiency, poor accuracy, and reliance on experience of traditional manual docking methods for fixed wing aircraft cabin segments, with the aim of developing an automated cabin docking system based on multimodal data fusion. By using multimodal data real-time acquisition technologies such as vision, distance measurement, and force sensors, combined with servo control and AI image processing algorithms, a three-stage automated docking process including axis alignment, radial docking, and control feedback was constructed, achieving precise adjustment and real-time monitoring of cabin pose. The hardware system design integrates high-precision sensors, a movable adjustable platform, and a comprehensive control board, and develops main control software to achieve multimodal data fusion and closed-loop control. Through automated docking tests, the system has successfully completed high-precision docking of different shaped cabin segments, significantly improving docking efficiency, reducing manual intervention by more than 90%, lowering collision risks, and meeting the engineering application requirements under complex working conditions. The results indicate that the system effectively improves docking consistency and reliability, providing an efficient solution for modular assembly of aircraft and suitable for docking tasks of different types and sizes of cabin segments. In addition, in response to the limitations of the existing system, directions have been proposed to further optimize the multi degree of freedom adjustment function.

    参考文献
    相似文献
    引证文献
引用本文

吴晓晔,胡志伟,唐晓田,白香雪,董旭,胡若愚.一种飞行器自动化舱段对接系统设计与实现计算机测量与控制[J].,2025,33(8):319-326.

复制
相关视频

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:2025-03-05
  • 最后修改日期:2025-04-16
  • 录用日期:2025-04-21
  • 在线发布日期: 2025-09-05
  • 出版日期:
文章二维码