基于视觉测量的民机PFD 状态量时序解析方法
DOI:
CSTR:
作者:
作者单位:

1.西北工业大学自动化学院西安710100; 2.中航民机机载系统工程中心有限公司上海201100

作者简介:

通讯作者:

中图分类号:

TH85TP391.41

基金项目:


Vision-based temporal analysis method for civil aircraft PFD states
Author:
Affiliation:

1.School of Automation, Northwestern Polytechnical University, Xi′an 710100, China; 2.AVIC Civil Aircraft Airborne System Engineering Center Co., Ltd., Shanghai 201100, 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:

    现有民机驾驶舱飞行任务中主飞行显示器(primary flight display, PFD)状态信息多依赖人工判读,其显示形态差异显著、界面信息密集,智能化提取难度较高,而机载数据接口常受权限管理、适航认证和平台开放性限制,基于外部相机的非接触式视觉感知具有较好的部署灵活性,提出一种基于视觉测量的PFD多状态量提取与时序修正方法,为飞行过程中的动作触发和辅助决策提供状态输入。首先,采用改进YOLOv8模型完成PFD区域识别与定位,并基于ORB特征匹配对显示界面进行透视校正,以提高状态解析的空间一致性。其次,针对PFD显示对象在视觉特征、颜色属性及几何构型上的差异构建状态解析策略,实现多类关键状态量的协同提取。此外,建立二阶常速度状态空间模型,结合序贯卡尔曼滤波与基于量测预测残差统计的异常检验机制,对状态量进行递推估计修正。基于X-Plane仿真环境和半实物驾驶舱平台的实验结果表明,所提算法能够获得较稳定的PFD定位结果,MCE、MWE和MHE分别为5.44、14.15和5.81 pixels。连续状态量估计中,空速、爬升率、气压高度和无线电高度的MAE/RMSE分别为0.06/0.08 kt、0.07/0.14、10.16/25.98 ft和1.55/1.98 ft,表明所提时序修正方法在受控半实物仿真条件下能够有效抑制异常感知,并提高PFD多状态量解析结果的时序稳定性。

    Abstract:

    In current civil aircraft cockpit flight tasks, primary flight display (PFD) state information is still mainly interpreted manually. Owing to the dense interface layout, diverse display forms, and limited accessibility of airborne data interfaces caused by permission management, airworthiness certification, and platform openness, external-camera-based non-contact visual perception provides a flexible solution for PFD state acquisition. This article proposes a vision-based method for PFD multi-state extraction and temporal correction to provide state inputs for action triggering and auxiliary decision-making during flight tasks. An improved YOLOv8 model is used for PFD region detection, followed by ORB-based perspective correction to improve the spatial consistency of state parsing. According to the visual features, color attributes, and geometric structures of different display elements, corresponding parsing strategies are designed to extract multiple key state variables. A second-order constant-velocity state-space model is further established, in which sequential Kalman filtering and residual-statistics-based anomaly detection are combined for recursive estimation and correction. Experiments conducted in an X-Plane-based semi-physical cockpit platform show that the proposed method achieves stable PFD localization, with MCE, MWE, and MHE of 5.44, 14.15, and 5.81 pixels, respectively. For continuous-state estimation, the MAE/RMSE values of airspeed, climb rate, barometric altitude, and radio altitude are 0.06/0.08 kt, 0.07/0.14, 10.16/25.98 ft, and 1.55/1.98 ft, respectively. The results show that the proposed temporal correction method can suppress abnormal observations and improve the temporal stability of PFD multi-state parsing under controlled semi-physical simulation conditions.

    参考文献
    相似文献
    引证文献
引用本文

王通,张嘉瑞,严恭敏,徐雨宁.基于视觉测量的民机PFD 状态量时序解析方法[J].仪器仪表学报,2026,47(8):303-316

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: 2026-10-29
  • 出版日期:
文章二维码