TY - GEN
T1 - Multi-Sensor Tracklet Association Considering Spatiotemporal Deviation Calibration
AU - Jiang, Yihang
AU - Cai, Han
AU - Zhang, Jingrui
AU - Gu, Xiansong
N1 - Publisher Copyright:
© 2024 International Astronautical Federation, IAF. All rights reserved.
PY - 2024
Y1 - 2024
N2 - The number of space objects increased exponentially in recent years due to the development of several LEO constellations and break-up events. Monitoring a large number of space objects using optical surveillance sensors may generate many short-arc observations, namely tracklets. Tracklet Association (TA) is a prerequisite for orbit determination, target identification, and catalog maintenance. However, a challenge emerges in the process of associating tracklets from multiple sensors, where some systematic spatiotemporal biases caused by environmental influences, time drift, and attitude positioning errors are always overlooked in applications. Consequently, biased data may lead to incorrect associations, while utilizing error-associated tracklets for spatiotemporal deviation correction may result in inaccurate outcomes. If the problem of multisensor TA and spatiotemporal deviation calibration can be resolved simultaneously, the accuracy of TA and orbit determination can be further enhanced. To overcome this challenge, this paper develops a multi-sensor TA and spatiotemporal calibration joint optimization method. The principle of optimization involves incorporating spatiotemporal biases as variables for optimization. The optimal solution is identified when a bias, added to measurements for compensation, maximizes the likelihood of associating tracklets within a reasonable limit. To this end, the likelihood of association is assessed through the Mahalanobis distance between the measured and estimated angular-rate information, where the latter can be generated through the Boundary Value Problem (BVP). For each hypothetical bias employed in optimization, a corresponding BVP can be established and addressed to evaluate whether such a bias confirms or rejects the association of the two tracklets. Therefore, a user-defined threshold can be applied to determine if the association and spatiotemporal deviation calibration are well accepted. The developed method is compared with the traditional TA methods using a simulation scenario. It considers the TA of 3 randomly selected space objects and 2 randomly selected space observers from the public catalog of the 18th Space Defense Squadron, the new approach demonstrates a consistent TA accuracy with traditional methods, affirming its effectiveness in typical scenarios.
AB - The number of space objects increased exponentially in recent years due to the development of several LEO constellations and break-up events. Monitoring a large number of space objects using optical surveillance sensors may generate many short-arc observations, namely tracklets. Tracklet Association (TA) is a prerequisite for orbit determination, target identification, and catalog maintenance. However, a challenge emerges in the process of associating tracklets from multiple sensors, where some systematic spatiotemporal biases caused by environmental influences, time drift, and attitude positioning errors are always overlooked in applications. Consequently, biased data may lead to incorrect associations, while utilizing error-associated tracklets for spatiotemporal deviation correction may result in inaccurate outcomes. If the problem of multisensor TA and spatiotemporal deviation calibration can be resolved simultaneously, the accuracy of TA and orbit determination can be further enhanced. To overcome this challenge, this paper develops a multi-sensor TA and spatiotemporal calibration joint optimization method. The principle of optimization involves incorporating spatiotemporal biases as variables for optimization. The optimal solution is identified when a bias, added to measurements for compensation, maximizes the likelihood of associating tracklets within a reasonable limit. To this end, the likelihood of association is assessed through the Mahalanobis distance between the measured and estimated angular-rate information, where the latter can be generated through the Boundary Value Problem (BVP). For each hypothetical bias employed in optimization, a corresponding BVP can be established and addressed to evaluate whether such a bias confirms or rejects the association of the two tracklets. Therefore, a user-defined threshold can be applied to determine if the association and spatiotemporal deviation calibration are well accepted. The developed method is compared with the traditional TA methods using a simulation scenario. It considers the TA of 3 randomly selected space objects and 2 randomly selected space observers from the public catalog of the 18th Space Defense Squadron, the new approach demonstrates a consistent TA accuracy with traditional methods, affirming its effectiveness in typical scenarios.
UR - http://www.scopus.com/inward/record.url?scp=85219165870&partnerID=8YFLogxK
U2 - 10.52202/078360-0183
DO - 10.52202/078360-0183
M3 - Conference contribution
AN - SCOPUS:85219165870
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 1897
EP - 1904
BT - 22nd IAA Symposium on Space Debris - Held at the 75th International Astronautical Congress, IAC 2024
PB - International Astronautical Federation, IAF
T2 - 22nd IAA Symposium on Space Debris at the 75th International Astronautical Congress, IAC 2024
Y2 - 14 October 2024 through 18 October 2024
ER -