Survey of highly non-Keplerian orbits with low-thrust propulsion

RJ McKay, M Macdonald, J Biggs… - Journal of Guidance …, 2011 - arc.aiaa.org
CELESTIAL mechanics has traditionally been concerned with orbital motion under the
action of a conservative gravitational potential. In particular, the inverse square gravitational …

Survey on advances in orbital dynamics and control for libration point orbits

M Xu, Y Liang, K Ren - Progress in Aerospace Sciences, 2016 - Elsevier
Libration point orbits (LPOs) have drawn a lot of interest because of their great significance
in deep space exploration. This paper summarizes the past developments and then …

Linearized relative motion and proximity control of E-sail-based displaced orbits

X Pan, AA Quarta, G Mengali, M Xu - Aerospace Science and Technology, 2020 - Elsevier
This paper discusses the linearized relative motion and control of Electric Solar Wind Sails
(E-sails) operating in formation flight around a heliocentric displaced orbit. An E-sail is …

On the existence of J 2 invariant relative orbits from the dynamical system point of view

M Xu, Y Wang, S Xu - Celestial Mechanics and Dynamical Astronomy, 2012 - Springer
The present paper addresses the existence of J 2 invariant relative orbits with arbitrary
relative magnitude over the infinite time using the Routh reduction and Poincaré techniques …

Magnetic sail-based displaced non-Keplerian orbits

M Bassetto, AA Quarta, G Mengali - Aerospace Science and Technology, 2019 - Elsevier
This paper deals with the problem of determining the requirements for the maintenance of
circular, displaced, non-Keplerian orbits around the Sun by means of a magnetic sail-based …

Artificial equilibrium points for a generalized sail in the circular restricted three-body problem

G Aliasi, G Mengali, AA Quarta - Celestial Mechanics and Dynamical …, 2011 - Springer
This paper introduces a new approach to the study of artificial equilibrium points in the
circular restricted three-body problem for propulsion systems with continuous and purely …

Formation flying on quasi-halo orbits in restricted Sun–Earth/Moon system

M Xu, Y Liang, X Fu - Aerospace Science and Technology, 2017 - Elsevier
Due to the strong nonlinear perturbations near the libration points, the continuous low-thrust
technique has many potential applications in stationkeeping relative motions. The …

Application of Hamiltonian structure-preserving control to formation flying on a J 2-perturbed mean circular orbit

M Xu, J Zhu, T Tan, S Xu - Celestial Mechanics and Dynamical Astronomy, 2012 - Springer
The bounded quasi-periodic relative trajectories are investigated in this paper for on-orbit
surveillance, inspection or repair, which requires rapid changes in formation configuration …

Displaced non-Keplerian orbits using impulsive thrust

CR McInnes - Celestial Mechanics and Dynamical Astronomy, 2011 - Springer
This paper investigates new families of displaced, highly non-Keplerian orbits in the two-
body problem and artificial equilibria in the circular restricted three-body problem. The …

A new constellation configuration scheme for communicating architecture in cislunar space

M Xu, J Wang, S Liu, S Xu - Mathematical Problems in …, 2013 - Wiley Online Library
A new constellation configuration is proposed to provide near‐constant communications
between any two points in the cislunar space. Four satellites were allocated on some natural …