Cited by 127Space Satellite Systems and ControlSpacecraft Dynamics and Control3D Shape Modeling and Analysis

Pose estimation for spacecraft relative navigation using model-based algorithms

Opromolla, Roberto, Fasano, Giancarmine, Rufino, Giancarlo, Grassi, Michele·2017·IEEE Transactions on Aerospace and Electronic Systems

Abstract

This paper presents the performance assessment of innovative model-based algorithms developed for pose estimation of uncooperative targets by processing sparse three-dimensional point clouds. This topic is of interest in the framework of advanced space applications, e.g., on-orbit servicing and active debris removal, which require a chaser spacecraft to execute autonomous relative navigation maneuvers in close-proximity of a space target. Both the problems of pose acquisition and tracking are addressed. The former one is carried out by combining the concepts of principal component analysis and template matching in order to limit both the computational effort and the amount of on-board data storage compared with traditional approaches. The latter is entrusted to a customized implementation of the iterative closest point algorithm, which adopts multiple model-measurement matching strategies as well as a refinement step, in order to respectively increase robustness and accelerate algorithm convergence. Also, safe transition from acquisition to tracking is implemented by means of autonomous detection of failures of the pose acquisition algorithm. The performance of the proposed techniques is investigated by means of numerical simulations in which the operation of an active LIDAR system as well as the target-chaser relative dynamics are realistically reproduced. Results demonstrate algorithms' effectiveness over a wide range of relative pose conditions and dealing with targets of variable size and shape, in spite of considerable sparseness of the measured datasets.

Integrity signals

Registry

Crossref · 10.1109/taes.2017.2650785

Cites

41 of 41 references verified0 citation errors · 0 not checkable

Statistics

Recomputing p-values needs the paper’s full text.

Claims the paper makes

This paper’s full text isn’t openly available, so its claims and self-check weren’t run. The registry and citation checks still apply.

Claims other papers make about this one

Each is checked against this paper’s own text: does it say what the citing paper says it does?

Cites

Flagged first, then by citations

Cited by

Sorted by citations

Authors
Opromolla, R., Fasano, G., Rufino, G., & Grassi, M.
Affiliations
University of Naples Federico II (IT)
Venue
IEEE Transactions on Aerospace and Electronic Systems
Published
2017-02
Volume
53
Issue
1
Pages
431-447
ISSN
0018-9251 (ISSN-L)
OpenAlex
W2568139125
Cited by
127
References
41
Citations by year
2026: 15 · 2025: 20 · 2024: 14 · 2023: 11 · 2022: 12 · 2021: 13 · 2020: 9 · 2019: 14 · 2018: 13 · 2017: 6
FWCI
10.57
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 › Computational Mechanics › 3D Shape Modeling and Analysis
Keywords
spacecraft relative navigation, pose estimation, non-cooperative targets, on-orbit servicing, active debris removal, chaser spacecraft, principal component analysis, template matching, iterative closest point, fault detection, LiDAR

About these checks

Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.

Statistics and arithmetic are recomputed, not judged.

Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.

What counts as a claim ›How we measure confidence ›How we check this ›

Are you an author, or do you see a problem with this page? Request a review