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基于多尺度ViT的航天器微损伤智能检测

马勇利 韩阅

航天器环境工程2025,Vol.42Issue(5):537-548,12.
航天器环境工程2025,Vol.42Issue(5):537-548,12.DOI:10.12126/see.2025044

基于多尺度ViT的航天器微损伤智能检测

Intelligent detection of spacecraft micro-damage based on multi-scale vision transformer

马勇利 1韩阅2

作者信息

  • 1. 北京卫星环境工程研究所
  • 2. 北京空间飞行器总体设计部:北京 100094
  • 折叠

摘要

Abstract

Spacecraft operating in complex space environments are susceptible to micro-scale surface damage,which poses threats to structural integrity and mission reliability.To overcome the limitations in scale modeling,feature alignment,and environmental adaptability of existing detection techniques,a novel spacecraft surface micro-damage detection method based on a dual-branch multi-scale Vision Transformer(ViT)is proposed.In the proposed architecture,global environmental context and local high-resolution detail features are extracted,and a saliency-guided fusion module(SGFM)is employed to dynamically aggregate critical regions and enhance the detection accuracy of minute damages.The method was evaluated on the Spacecraft-DS dataset for impurity and scratch detection on metallic housings within an end-to-end training framework.Compared with mainstream models such as YOLO-V8 and DETR,the proposed approach achieved improvements of up to 2.2%in APall,Recall,and F1,and reached an inference speed of 25 FPS.Superior performance was observed particularly in small-sized damage recognition and complex-background suppression,effectively addressing the limited receptive field of traditional CNNs and the scale-adaptability issues of standard ViTs.The results demonstrate that the proposed method provides an efficient technical solution for applications such as space-station inspection and satellite degradation analysis.

关键词

航天器表面微损伤/智能检测/双分支多尺度ViT/语义门控特征融合/小目标检测/航天器健康管理

Key words

spacecraft surface micro-damage/intelligent detection/dual-branch multi-scale vision transformer(ViT)/semantic-gated feature fusion/small-target detection/spacecraft health management

分类

航空航天

引用本文复制引用

马勇利,韩阅..基于多尺度ViT的航天器微损伤智能检测[J].航天器环境工程,2025,42(5):537-548,12.

航天器环境工程

1673-1379

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