The paper introduces a satellite-terrestrial cooperative routing framework that consists of a mega LEO satellite constellation and a small number of ground relays. To achieve accurate and low-complexity minimum end-to-end hop-count estimation in this cooperative routing scenario, the authors first design a satellite real-time position based graph (RTPG) to simplify the description of the 3D constellation. They then abstract RTPG into a key node based graph (KNBG) and develop a low-complexity generation method for KNBG. Finally, utilizing KNBG as input, the authors design the minimum end-to-end hop-count estimation method (KNBG-MHCE).
The proposed distributed satellite-terrestrial cooperative routing strategy makes routing decisions by jointly considering the minimum end-to-end hop-count constraints given by KNBG-MHCE and the load status of the current satellite queues as well as the next-hop node. The authors also analyze the computational complexity, routing path survival probability, and practical implementation of their proposal. Extensive simulations are conducted in systems with Ka and laser band inter-satellite links to verify the superiority of the proposed approach.
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