Solar sail technology—A state of the art review

B Fu, E Sperber, F Eke - Progress in Aerospace Sciences, 2016 - Elsevier
In this paper, the current state of the art of solar sail technology is reviewed. Solar sail
research is quite broad and multi-disciplinary; this paper focuses mainly on areas such as …

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 …

[HTML][HTML] Stochastic optimization for stationkeeping of periodic orbits using a high-order Target Point Approach

X Fu, N Baresi, R Armellin - Advances in Space Research, 2022 - Elsevier
Periodic orbits in the Restricted Three-Body Problem are widely adopted as nominal
trajectories by different missions. To maintain periodic orbits in a three-body regime, a …

Quaternion-based adaptive attitude control of asteroid-orbiting spacecraft via immersion and invariance

KW Lee, SN Singh - Acta Astronautica, 2020 - Elsevier
The design of an attitude control system for an asteroid-orbiting satellite via immersion and
invariance is the subject of this paper. It is assumed that the asteroid is rotating with a …

Stationkeeping Analysis for Solar Sailing the Region of Binary Asteroid Systems

D Guzzetti, R Sood, L Chappaz, H Baoyin - Journal of Guidance …, 2019 - arc.aiaa.org
Asteroid exploration may largely benefit from solar-sail propulsion that is coupled with
satellite miniaturization. There remain, however, several open questions on sail dynamics in …

High order dynamical systems approaches for low-thrust station-keeping of libration point orbits

C Gao, JJ Masdemont, G Gómez, J Chen, J Yuan - Acta Astronautica, 2022 - Elsevier
We derive two families of low-thrust station-keeping control procedures based on the
dynamical properties of the phase space near libration point orbits. The first family is …

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 …

Solar radiation pressure Hamiltonian feedback control for unstable libration-point orbits

S Soldini, C Colombo, SJI Walker - Journal of Guidance, Control, and …, 2017 - arc.aiaa.org
This work investigates a Hamiltonian structure-preserving control that uses the acceleration
of solar radiation pressure for the stabilization of unstable periodic orbits in the circular …

Trajectory optimization for solar sail in cislunar navigation constellation with minimal lightness number

X Pan, M Xu, R Santos - Aerospace Science and Technology, 2017 - Elsevier
In view of the limitations of the existing libration-point satellite navigation systems in cislunar
space, this paper replaces satellites with solar sails to construct a cislunar navigation …

Formation flying along halo orbit of circular-restricted three-body problem

M Bando, A Ichikawa - Journal of Guidance, Control, and Dynamics, 2015 - arc.aiaa.org
STATIONKEEPING on a unstable orbit in the circular-restiricted three-body problem
(CR3BP) has been studied by many authors [1–5]. There are two types of strategy [5] …