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astro-ph.IM2026
Rapid Sequence Cost Evaluation for Multi-Spacecraft Rendezvous: A Permutation-Invariant Set Transformer
An-yi Huang
Multi-spacecraft multi-rendezvous mission design requires repeated evaluations of the total cost of visiting a target set within a given time window, and the efficiency of this eva…
astro-ph.IM2026
HELIOS: An LLM-Driven Autonomous Indirect Trajectory Optimization Agent
An-yi Huang
Low-thrust trajectory optimization is a core technology in deep-space mission design. Indirect methods based on Pontryagin's Minimum Principle (PMP) offer rigorous optimality guara…
astro-ph.IM2022★ 6 cited
Simplified Optimization Model for Low-Thrust Perturbed Rendezvous Between Low-Eccentricity Orbits
An-yi Huang, Heng-nian Li
Trajectory optimization of low-thrust perturbed orbit rendezvous is a crucial technology for space missions in low Earth orbits, which is difficult to solve due to its initial valu…