This paper presents the trajectory design for EQUilibriUm Lunar-Earth point 6U Spacecraft
(EQUULEUS), which aims to demonstrate orbit control capability of CubeSats in the cislunar …

Classically, space situational awareness (SSA) and space traffic management (STM) focus
on the near-Earth region, which is highly populated by satellites and space debris objects …

Stable or nearly stable orbits do not generally possess well-distinguished manifold
structures that assist in designing trajectories for departing from or arriving onto a periodic …

The Keplerian orbital elements make up a set of parameters that uniquely describe a two-
body trajectory. Once perturbations are imposed on two-body dynamics, one often studies …

The Lunar Meteoroid Impacts Observer, or LUMIO, is a space mission concept awarded
winner of ESA's SysNova Competition “Lunar CubeSats for Exploration,” and as such it is …

Designing trajectories in dynamically complex environments is challenging and easily
becomes intractable. Recasting the problem may reduce the design time and offer global …

A dynamical understanding of orbits in the Earth-Moon neighborhood that can sustain long-
term activities and trajectories that link locations of interest forms a critical foundation for the …

In the near future, several space applications in the Earth-Moon system may require a
spacecraft to hold a stable motion, but the transfer trajectory infrastructure to access such …

A multiple grid search strategy is implemented to generate a broad database of
axisymmetric three-body periodic orbits for planets and main planetary satellites in the Solar …

This document reflects the effort of constructing a basis for understanding attitude motion
within a multi-body problem with application to spacecraft flight dynamics. The circular …