Robust template feature matching method using motion-constrained DCF designed for visual navigation in asteroid landing

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS
Yaqiong Wang, Xiongfeng Yan, Zhen Ye, Huan Xie, Shijie Liu, Xiong Xu, Xiaohua Tong
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引用次数: 0

Abstract

A robust and efficient feature matching method is necessary for visual navigation in asteroid-landing missions. Based on the visual navigation framework and motion characteristics of asteroids, a robust and efficient template feature matching method is proposed to adapt to feature distortion and scale change cases for visual navigation of asteroids. The proposed method is primarily based on a motion-constrained discriminative correlation filter (DCF). The prior information provided by the motion constraints between sequence images is used to provide a predicted search region for template feature matching. Additionally, some specific template feature samples are generated using the motion constraints for correlation filter learning, which is beneficial for training a scale and feature distortion adaptive correlation filter for accurate feature matching. Moreover, average peak-to-correlation energy (APCE) and jointly consistent measurements (JCMs) were used to eliminate false matching. Images captured by the Touch And Go Camera System (TAGCAMS) of the Bennu asteroid were used to evaluate the performance of the proposed method. In particular, both the robustness and accuracy of region matching and template center matching are evaluated. The qualitative and quantitative results illustrate the advancement of the proposed method in adapting to feature distortions and large-scale changes during spacecraft landing.

基于运动约束的DCF鲁棒模板特征匹配方法设计用于小行星着陆视觉导航
一种鲁棒、高效的特征匹配方法是实现小行星着陆任务视觉导航的必要条件。基于视觉导航框架和小行星的运动特征,提出了一种鲁棒高效的模板特征匹配方法,以适应小行星视觉导航中特征失真和尺度变化的情况。该方法主要基于运动约束判别相关滤波器(DCF)。利用序列图像之间运动约束提供的先验信息为模板特征匹配提供预测搜索区域。此外,利用运动约束生成特定模板特征样本进行相关滤波器学习,有利于训练尺度和特征失真自适应的相关滤波器,实现准确的特征匹配。此外,使用平均峰相关能(APCE)和联合一致测量(JCMs)来消除错误匹配。使用Bennu小行星的触控相机系统(TAGCAMS)拍摄的图像来评估所提出方法的性能。特别对区域匹配和模板中心匹配的鲁棒性和准确性进行了评价。定性和定量结果表明了该方法在适应航天器着陆过程中特征畸变和大尺度变化方面的进步。
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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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