TY - GEN
T1 - Artificial Intelligence-Assisted Spacecraft Swarm Reconfiguration Planning
AU - Zhu, Tianhao
AU - Qiao, Dong
AU - Han, Hongwei
N1 - Publisher Copyright:
© 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
PY - 2023
Y1 - 2023
N2 - Nowadays, the spacecraft swarm reconfiguration planning method of large-scale spacecraft generally faces the disadvantages of complex constraints and long calculation time, which limits the scale of spacecraft swarm in practical applications. In order to reduce the time of spacecraft swarm reconfiguration planning, this paper proposes an artificial intelligence-assisted rapid swarm reconfiguration planning method: the method first uses the Latin Hypercube Sampling method to obtain sample points and trains the BP neural network. Based on the pre-trained neural network, one can estimate the minimum distance between each spacecraft and identify the interval where collisions may occur. Finally, the convex optimization method is used to solve the swarm reconfiguration problem. The effectiveness of the method is verified by solving the 100- satellite formation reconstruction problem. The simulation results show that the number of collision constraints is reduced from 4950 to 155, and the solution time of the planning problem is about 20 s. Numerical simulation proves that the method proposed in this paper can effectively reduce the dimensionality of the large-scale cluster spacecraft reconstruction planning problem and has the potential for practical application.
AB - Nowadays, the spacecraft swarm reconfiguration planning method of large-scale spacecraft generally faces the disadvantages of complex constraints and long calculation time, which limits the scale of spacecraft swarm in practical applications. In order to reduce the time of spacecraft swarm reconfiguration planning, this paper proposes an artificial intelligence-assisted rapid swarm reconfiguration planning method: the method first uses the Latin Hypercube Sampling method to obtain sample points and trains the BP neural network. Based on the pre-trained neural network, one can estimate the minimum distance between each spacecraft and identify the interval where collisions may occur. Finally, the convex optimization method is used to solve the swarm reconfiguration problem. The effectiveness of the method is verified by solving the 100- satellite formation reconstruction problem. The simulation results show that the number of collision constraints is reduced from 4950 to 155, and the solution time of the planning problem is about 20 s. Numerical simulation proves that the method proposed in this paper can effectively reduce the dimensionality of the large-scale cluster spacecraft reconstruction planning problem and has the potential for practical application.
KW - BP neural network
KW - Reconstruction planning
KW - Spacecraft swarm
UR - http://www.scopus.com/inward/record.url?scp=85135864940&partnerID=8YFLogxK
U2 - 10.1007/978-981-19-3998-3_56
DO - 10.1007/978-981-19-3998-3_56
M3 - Conference contribution
AN - SCOPUS:85135864940
SN - 9789811939976
T3 - Lecture Notes in Electrical Engineering
SP - 583
EP - 592
BT - Proceedings of 2021 5th Chinese Conference on Swarm Intelligence and Cooperative Control
A2 - Ren, Zhang
A2 - Hua, Yongzhao
A2 - Wang, Mengyi
PB - Springer Science and Business Media Deutschland GmbH
T2 - 5th Chinese Conference on Swarm Intelligence and Cooperative Control, CCSICC 2021
Y2 - 19 January 2022 through 22 January 2022
ER -