Statistical Analysis of the Role of Invariant Manifolds on Robust Trajectories

A Sinha, R Beeson - arxiv preprint arxiv:2409.19905, 2024 - arxiv.org
As low-thrust space missions increase in prevalence, it is becoming increasingly important
to design robust trajectories against unforeseen thruster outages or missed thrust events …

Initial Guess Generation for Low-Thrust Trajectory Design with Robustness to Missed-Thrust-Events

A Sinha, R Beeson - arxiv preprint arxiv:2501.06694, 2025 - arxiv.org
The growing interest in cislunar space exploration in recent years has driven an increasing
demand for efficient low-thrust missions to key cislunar orbits. These missions, typically …

Global Search for Optimal Low Thrust Spacecraft Trajectories using Diffusion Models and the Indirect Method

J Graebner, R Beeson - arxiv preprint arxiv:2501.07005, 2025 - arxiv.org
Long time-duration low-thrust nonlinear optimal spacecraft trajectory global search is a
computationally and time expensive problem characterized by clustering patterns in locally …

Algorithmic Considerations for Effective Global Search of Robust Low-Thrust Trajectories

A Sinha, R Beeson - arxiv preprint arxiv:2410.00297, 2024 - arxiv.org
The growing interest in the cislunar domain over the past decade has led to an increasing
demand for low-thrust missions to key orbits within this region. These low-thrust missions …

[PDF][PDF] GLOBAL ANALYSIS OF OPTIMAL TRAJECTORIES FROM EARTH-MOON 9: 2 NEAR RECTILINEAR HALO ORBIT TO LOW-LUNAR ORBITS

SG Jo, A Sinha, M Palomo, J Graebner, A Anderson… - researchgate.net
NASA's Gateway station in the 9: 2 near-rectilinear halo orbit (NRHO) will facilitate missions
to dock in the cislunar realm before landing on the Lunar surface. Designing a transfer …