[HTML][HTML] Research advancements in key technologies for space-based situational awareness

B Wang, S Li, J Mu, X Hao, W Zhu… - Space: Science & …, 2022 - spj.science.org
The space environment has become highly congested due to the increasing space debris,
seriously threatening the safety of orbiting spacecraft. Space-based situational awareness …

[HTML][HTML] Survey of orbital dynamics and control of space rendezvous

Y Luo, J Zhang, G Tang - Chinese Journal of Aeronautics, 2014 - Elsevier
Rendezvous orbital dynamics and control (RODC) is a key technology for operating space
rendezvous and docking missions. This paper surveys the studies on RODC. Firstly, the …

Kalman filtering for relative spacecraft attitude and position estimation

SG Kim, JL Crassidis, Y Cheng, AM Fosbury… - Journal of Guidance …, 2007 - arc.aiaa.org
In this paper a novel approach is developed for relative state estimation of spacecraft flying
in formation. The approach uses information from an optical sensor to provide multiple line …

Stereovision-based pose and inertia estimation of unknown and uncooperative space objects

V Pesce, M Lavagna, R Bevilacqua - Advances in Space Research, 2017 - Elsevier
Autonomous close proximity operations are an arduous and attractive problem in space
mission design. In particular, the estimation of pose, motion and inertia properties of an …

Periodic solution of the nonlinear Sitnikov restricted three-body problem

EI Abouelmagd, JLG Guirao, AK Pal - New Astronomy, 2020 - Elsevier
The objective of this paper is to find periodic solutions of the circular Sitnikov problem by the
multiple scales method which is used to remove the secular terms and find the periodic …

Manifolds and metrics in the relative spacecraft motion problem

P Gurfil, KV Kholshevnikov - Journal of guidance, control, and dynamics, 2006 - arc.aiaa.org
MODELING relative spacecraft motion is of prime importance for formation-flying satellites
and distributed spacecraft systems, which constitute a significant share of planned future …

Relative motion and the geometry of formations in Keplerian elliptic orbits with arbitrary eccentricity

P Sengupta, SR Vadali - Journal of guidance, control, and dynamics, 2007 - arc.aiaa.org
The well-known Hill–Clohessy–Wiltshire equations that are used for the design of formation
flight relative orbits are based on a circular reference orbit. Classical solutions such as the …

Classical element feedback control for spacecraft orbital maneuvers

BJ Naasz - 2002 - vtechworks.lib.vt.edu
The recent addition of autonomous formation flying spacecraft to the world's satellite fleet
provides new motivation to study feedback control techniques. In this thesis, we develop …

Second-order state transition for relative motion near perturbed, elliptic orbits

P Sengupta, SR Vadali, KT Alfriend - Celestial Mechanics and Dynamical …, 2007 - Springer
This paper develops a tensor and its inverse, for the analytical propagation of the position
and velocity of a satellite, with respect to another, in an eccentric orbit. The tensor is useful …

Periodic solutions of nonlinear relative motion satellites

AK Pal, EI Abouelmagd, JL García Guirao… - Symmetry, 2021 - mdpi.com
The relative motion of an outline of the rendezvous problem has been studied by assuming
that the chief satellite is in circular symmetric orbits. The legitimacy of perturbation …