TY - JOUR
T1 - Rapid On-Orbit Repair Mission Planning for Multiple GEO Spacecraft Based on a Mixed Repair Strategy
AU - Yan, Huida
AU - Yuan, Li
AU - Li, Chuanjiang
AU - Guo, Yanning
AU - Ran, Guangtao
AU - Wang, Bo Hui
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2025
Y1 - 2025
N2 - This study focuses on mission planning for repairing multiple damaged spacecraft in geosynchronous orbit (GEO). A mixed repair strategy is proposed, including using a single service spacecraft (SSc), simultaneous repair by two SScs, and repair within a space station (SS). We employ hybrid propulsion to reduce fuel consumption. The optimization objective is to minimize mission duration, aiming for the fastest possible repair to restore the damaged spacecraft's functionality. The SSc-SS-target spacecraft repair mission planning model is established, considering practical constraints such as spacecraft maneuverability, fuel capacity, service sequence conflict, etc. A two-level solution framework is presented: the upper level applies a genetic algorithm (GA) to solve for the allocation method, service sequence, and repair strategy, with enhanced optimization efficiency through a local search (LS) strategy. In addition, graph theory is applied to resolve sequence conflicts and ensure the strategy's feasibility. The lower level uses variable neighborhood search (VNS) to optimize the maneuver trajectory. Finally, representative simulations and comparative examples validate the proposed solution framework.
AB - This study focuses on mission planning for repairing multiple damaged spacecraft in geosynchronous orbit (GEO). A mixed repair strategy is proposed, including using a single service spacecraft (SSc), simultaneous repair by two SScs, and repair within a space station (SS). We employ hybrid propulsion to reduce fuel consumption. The optimization objective is to minimize mission duration, aiming for the fastest possible repair to restore the damaged spacecraft's functionality. The SSc-SS-target spacecraft repair mission planning model is established, considering practical constraints such as spacecraft maneuverability, fuel capacity, service sequence conflict, etc. A two-level solution framework is presented: the upper level applies a genetic algorithm (GA) to solve for the allocation method, service sequence, and repair strategy, with enhanced optimization efficiency through a local search (LS) strategy. In addition, graph theory is applied to resolve sequence conflicts and ensure the strategy's feasibility. The lower level uses variable neighborhood search (VNS) to optimize the maneuver trajectory. Finally, representative simulations and comparative examples validate the proposed solution framework.
KW - Geosynchronous orbit (GEO)
KW - local search (LS)
KW - mixed repair strategy
KW - on-orbit repair mission planning
KW - two-level solution framework
UR - https://www.scopus.com/pages/publications/85201768166
U2 - 10.1109/TAES.2024.3445318
DO - 10.1109/TAES.2024.3445318
M3 - 文章
AN - SCOPUS:85201768166
SN - 0018-9251
VL - 61
SP - 279
EP - 295
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 1
ER -