Cited by 101Space Satellite Systems and ControlSpacecraft Dynamics and ControlSatellite Image Processing and Photogrammetry

Relative pose estimation for cylinder-shaped spacecrafts using single image

Liu, Chang, Hu, Weiduo·2014·IEEE Transactions on Aerospace and Electronic Systems

Abstract

This paper describes a novel framework to determine the relative pose and range of a solid-of-revolution-shaped spacecraft from a single image without any artificial beacons. The translation and the symmetry axis of the spacecraft can be estimated from the imaged cross sections of the spacecraft body. Then the pose and range of the spacecraft are fully determined by means of the images of its solar panels and asymmetric feature. Our method has been validated by both synthetic and real images.

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Crossref · 10.1109/taes.2014.120757

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49 of 49 references verified0 citation errors · 0 not checkable

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Authors
Liu, C., & Hu, W.
Affiliations
Beihang University (CN)
Venue
IEEE Transactions on Aerospace and Electronic Systems
Published
2014-10
Volume
50
Issue
4
Pages
3036-3056
ISSN
0018-9251 (ISSN-L)
OpenAlex
W2064607980
Cited by
101
References
49
Citations by year
2026: 5 · 2025: 9 · 2024: 9 · 2023: 14 · 2022: 9 · 2021: 10 · 2020: 8 · 2019: 14 · 2018: 13 · 2017: 5 · 2016: 3 · 2015: 1 · 2014: 1
FWCI
4.92
Type
journal article
Language
en
Open access
closed
Locations
IEEE Transactions on Aerospace and Electronic Systems (publishedVersion)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Space Satellite Systems and Control
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
  • Physical Sciences › Engineering › Ocean Engineering › Satellite Image Processing and Photogrammetry
Keywords
relative pose estimation, single image, solids of revolution, solar panels, cross-section images

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