TY - GEN
T1 - A Semi-analytical Stable Formation Configuration Screening Method Based on Poincaré Contraction Map
AU - Ding, Jixin
AU - Pan, Xiao
AU - Bai, Xue
AU - Xu, Ming
N1 - Publisher Copyright:
Copyright © 2025 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2025
Y1 - 2025
N2 - This paper proposes a semi-analytical method integrating Poincaré Compressed Mapping (PCM) with Conditional Variational Autoencoder (CVAE) for efficient screening of bounded relative orbit. PCM is applied to reduce the four-dimensional state parameters to a two-dimensional feature parameter pair of crossing period and separation angle, which is surjective but non-injective. In the feature parameter plane, contour maps of the state parameters are constructed, whose intersections correspond to long-duration formation with limited amplitude. However, this ergodic search method suffers from high computational cost and low flexibility, which can be simplified into an inverse mapping from the chief’s feature parameters to the deputy’s state parameters for rapid configuration screening. Therefore, a semi-analytical PCM-CVAE method is developed for dimensional raising from the two-dimensional feature parameters of the chief to the four-dimensional state parameters of the deputy, enabling diverse screening of feasible bounded relative orbits. Results under the displaced orbit scenario demonstrate that PCM-CVAE method achieves an optimal accuracy of (1.92×10-4, 5.94×10-4), while reducing the search time from the hour level to 7.83 minutes.
AB - This paper proposes a semi-analytical method integrating Poincaré Compressed Mapping (PCM) with Conditional Variational Autoencoder (CVAE) for efficient screening of bounded relative orbit. PCM is applied to reduce the four-dimensional state parameters to a two-dimensional feature parameter pair of crossing period and separation angle, which is surjective but non-injective. In the feature parameter plane, contour maps of the state parameters are constructed, whose intersections correspond to long-duration formation with limited amplitude. However, this ergodic search method suffers from high computational cost and low flexibility, which can be simplified into an inverse mapping from the chief’s feature parameters to the deputy’s state parameters for rapid configuration screening. Therefore, a semi-analytical PCM-CVAE method is developed for dimensional raising from the two-dimensional feature parameters of the chief to the four-dimensional state parameters of the deputy, enabling diverse screening of feasible bounded relative orbits. Results under the displaced orbit scenario demonstrate that PCM-CVAE method achieves an optimal accuracy of (1.92×10-4, 5.94×10-4), while reducing the search time from the hour level to 7.83 minutes.
KW - CVAE Algorithm
KW - Formation Congiguration
KW - Poincaré Map
KW - Spacecraft Formation Flying
UR - https://www.scopus.com/pages/publications/105036336139
U2 - 10.52202/083087-0078
DO - 10.52202/083087-0078
M3 - 会议稿件
AN - SCOPUS:105036336139
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 923
EP - 933
BT - IAF Astrodynamics Symposium - Held at the 76th International Astronautical Congress, IAC 2025
PB - International Astronautical Federation, IAF
T2 - 2025 IAF Astrodynamics Symposium at the 76th International Astronautical Congress, IAC 2025
Y2 - 29 September 2025 through 3 October 2025
ER -