TY - GEN
T1 - Probabilistic Tracklet Clustering and Initial Orbit Determination
AU - Jiang, Yihang
AU - Cai, Han
AU - Yang, Yang
AU - Zhang, Jingrui
AU - Ju, Bing
AU - Liu, Ying
N1 - Publisher Copyright:
© 2025 International Astronautical Federation, IAF. All rights reserved.
PY - 2025
Y1 - 2025
N2 - Space Situational Awareness (SSA) is critical for monitoring the increasing number of space objects. A key component of SSA is tracklet clustering, which involves integrating fragmented observation data from multiple sensors to construct continuous trajectories. Effective tracklet clustering facilitates object identification and initial orbit determination (IOD), thereby enhancing collision avoidance and space traffic management. The primary challenge in tracklet clustering is managing the vast volume of observation data. Deploying mega-constellations has significantly expanded the number of observable space objects. Traditional approaches struggle to establish accurate correlations within such large datasets, particularly in the case of constellation satellites. Moreover, optical tracklets frequently arise from short observation arcs, leading to significant uncertainty in angular velocity, which further complicates the association of multiple tracklets with a single object. To overcome these challenges, this paper develops a probabilistic tracklet clustering method and a robust IOD method based on clustering. The process begins with an initial association executed via the Boundary Value Problem-Constrained Admissible Region Optimization method (BVP-CAR-Opt). The association probability between two tracklets is assessed through the Mahalanobis distance between the measured and estimated angular-rate information. The tracklet clustering is formulated as an optimization problem. The optimization objective is to maximize the likelihood of the association matrix, which is calculated based on the association probabilities obtained through the BVP-CAR-Opt method. This progress achieves efficient and accurate tracklet clustering by solving the optimal association matrix, avoiding the exhaustive enumeration of all hypotheses. Once the clusters are determined, the weighted hypothetical orbits are generated by the BVP-CAR-Opt according to their corresponding association probabilities. These weighted hypothetical orbits are subsequently utilized in the least squares algorithm to yield the initial orbit. Incorporating weighting factors significantly reduces the relative influence of the assumed orbits on error estimation, thereby ensuring a stable and consistent initial orbit. To evaluate the performance of the developed method, one simulation scenario was employed and compared with Markov clustering techniques. Optical observation data were generated from a LEO space-based sensor. The tracklet clustering was applied to 30 randomly selected space objects from the 18th Space Defense Squadron public catalog. The new approach demonstrates a higher tracklet clustering accuracy compared with Markov clustering, affirming its effectiveness in typical scenarios.
AB - Space Situational Awareness (SSA) is critical for monitoring the increasing number of space objects. A key component of SSA is tracklet clustering, which involves integrating fragmented observation data from multiple sensors to construct continuous trajectories. Effective tracklet clustering facilitates object identification and initial orbit determination (IOD), thereby enhancing collision avoidance and space traffic management. The primary challenge in tracklet clustering is managing the vast volume of observation data. Deploying mega-constellations has significantly expanded the number of observable space objects. Traditional approaches struggle to establish accurate correlations within such large datasets, particularly in the case of constellation satellites. Moreover, optical tracklets frequently arise from short observation arcs, leading to significant uncertainty in angular velocity, which further complicates the association of multiple tracklets with a single object. To overcome these challenges, this paper develops a probabilistic tracklet clustering method and a robust IOD method based on clustering. The process begins with an initial association executed via the Boundary Value Problem-Constrained Admissible Region Optimization method (BVP-CAR-Opt). The association probability between two tracklets is assessed through the Mahalanobis distance between the measured and estimated angular-rate information. The tracklet clustering is formulated as an optimization problem. The optimization objective is to maximize the likelihood of the association matrix, which is calculated based on the association probabilities obtained through the BVP-CAR-Opt method. This progress achieves efficient and accurate tracklet clustering by solving the optimal association matrix, avoiding the exhaustive enumeration of all hypotheses. Once the clusters are determined, the weighted hypothetical orbits are generated by the BVP-CAR-Opt according to their corresponding association probabilities. These weighted hypothetical orbits are subsequently utilized in the least squares algorithm to yield the initial orbit. Incorporating weighting factors significantly reduces the relative influence of the assumed orbits on error estimation, thereby ensuring a stable and consistent initial orbit. To evaluate the performance of the developed method, one simulation scenario was employed and compared with Markov clustering techniques. Optical observation data were generated from a LEO space-based sensor. The tracklet clustering was applied to 30 randomly selected space objects from the 18th Space Defense Squadron public catalog. The new approach demonstrates a higher tracklet clustering accuracy compared with Markov clustering, affirming its effectiveness in typical scenarios.
UR - https://www.scopus.com/pages/publications/105040750780
U2 - 10.52202/083079-0064
DO - 10.52202/083079-0064
M3 - Conference contribution
AN - SCOPUS:105040750780
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 642
EP - 651
BT - 23rd IAA Symposium on Space Debris - Held at the 76th International Astronautical Congress, IAC 2025
PB - International Astronautical Federation, IAF
T2 - 23rd IAA Symposium on Space Debris at the 76th International Astronautical Congress, IAC 2025
Y2 - 29 September 2025 through 3 October 2025
ER -