This study was done to investigate the effect of perturbations of both oblate massive
primaries on the periodic orbit-attitude behavior of satellites at the three-body problem …

The hopping dynamics of a lander in single-tidal-locked binary asteroid systems is explored.
A coupled orbit-attitude dynamical model of the lander in the body-fixed frame of the …

The motion of a spacecraft in proximity to a small body is significantly perturbed due to its
irregular gravity field and solar radiation pressure. In such a strongly perturbed environment …

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 …

Trajectory design increasingly leverages multi-body dynamical structures that are based on
an understanding of various types of orbits in the Circular Restricted Three-Body Problem …

The gravitational coupling of the orbit and attitude motions of a large flexible solar power
satellite (SPS) is studied in this paper. The orbital and attitude dynamical equations of a SPS …

A space station in the vicinity of the Moon can be exploited as a gateway for future human
and robotic exploration of the solar system. The natural location for a space system of this …

Predicting the attitude of spacecraft traveling within the Cislunar region is crucial to ensure
the success of future missions planned within that realm of space. To consider the coupled …

This paper addresses the problem of spacecraft attitude and position synchronization in
libration point orbits between a leader and a follower. Using dual quaternion, the …

This study investigated periodic coupled orbit—attitude motions within the perturbed circular
restricted three-body problem (P-CRTBP) concerning the perturbations of a radiated …