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20212026
most citedSimplified Optimization Model for Low-Thrust Perturbed Rendezvous Between Low-Eccentricity Orbits

6 citations · 6 across the 4 of their papers we have counts for

collaborators

5 papers

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.EP2024

Analytical Delta-V Approximation for Nonlinear Programming of Multi-target Rendezvous and Flyby Trajectories

An-Yi Huang, Heng-Nian Li, Ya-Zhong Luo

This study proposes an analytical Delta-V approximation of short-time transfers based on the linear relative motion and a gradient-based nonlinear programming model of multi-target…

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…

nlin.CD2021

Fast Optimization of Impulsive Perturbed Orbit Rendezvous with Finite Iterations

An-yi Huang, Ya-zhong Luo, Heng-nian Li

A novel fast multi-impulse optimization method for long-duration perturbed orbit rendezvous is proposed. First, based on the analytically estimated impulses, the terminal rendezvou…