TY - JOUR
T1 - LEO Internet Satellite Constellation Design for Regional Civil Aviation Airways With Multiple Repeat Ground Tracks
AU - Han, Peng
AU - Li, Chuanjiang
AU - Huang, Chao
AU - Huang, Hailong
AU - Guo, Yanning
AU - Pan, Gaofeng
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2025
Y1 - 2025
N2 - The lack of Internet access significantly impacts the passenger experience on commercial airlines, necessitating reliable, high-throughput communication support. One promising solution is leveraging the satellite constellation in low Earth orbit (LEO). This article studies the design of an Internet satellite constellation in LEO for continuous communication coverage of regional airway targets. To address the problem, multiple repeat ground tracks (RGT) with the same period ratio are used as the reference. A mixed-integer simultaneous orbit optimization and satellite deployment model is established to minimize the number of satellites while satisfying the coverage requirement. A two-stage optimization framework is proposed to solve the problem with nonlinear and nonconvex constraints. In the first stage, differential evolution optimizes the parameters of each RGT orbit by minimizing the lower bound of the multiRGT orbit satellite deployment model. By leveraging the result in the first stage, the access profile is obtained, and the optimal satellite deployment result is derived in the second stage. Finally, detailed validation and comparison simulations are conducted based on three case studies to verify the effectiveness and superiority of the proposed model and algorithm.
AB - The lack of Internet access significantly impacts the passenger experience on commercial airlines, necessitating reliable, high-throughput communication support. One promising solution is leveraging the satellite constellation in low Earth orbit (LEO). This article studies the design of an Internet satellite constellation in LEO for continuous communication coverage of regional airway targets. To address the problem, multiple repeat ground tracks (RGT) with the same period ratio are used as the reference. A mixed-integer simultaneous orbit optimization and satellite deployment model is established to minimize the number of satellites while satisfying the coverage requirement. A two-stage optimization framework is proposed to solve the problem with nonlinear and nonconvex constraints. In the first stage, differential evolution optimizes the parameters of each RGT orbit by minimizing the lower bound of the multiRGT orbit satellite deployment model. By leveraging the result in the first stage, the access profile is obtained, and the optimal satellite deployment result is derived in the second stage. Finally, detailed validation and comparison simulations are conducted based on three case studies to verify the effectiveness and superiority of the proposed model and algorithm.
KW - Civil aviation airways
KW - low Earth orbit (LEO)
KW - repeat ground track (RGT) orbit
KW - satellite constellation design
UR - http://www.scopus.com/inward/record.url?scp=105002680429&partnerID=8YFLogxK
U2 - 10.1109/TAES.2024.3502002
DO - 10.1109/TAES.2024.3502002
M3 - Article
AN - SCOPUS:105002680429
SN - 0018-9251
VL - 61
SP - 4088
EP - 4104
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 2
ER -