Statistical Analysis of the Role of Invariant Manifolds on Robust Trajectories
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 …
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
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 …
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
Long time-duration low-thrust nonlinear optimal spacecraft trajectory global search is a
computationally and time expensive problem characterized by clustering patterns in locally …
computationally and time expensive problem characterized by clustering patterns in locally …
Algorithmic Considerations for Effective Global Search of Robust Low-Thrust Trajectories
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 …
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
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 …
to dock in the cislunar realm before landing on the Lunar surface. Designing a transfer …