Path planning and guidance algorithms for SAR formation reconfiguration: Comparison between centralized and decentralized approaches

S Sarno, M D'Errico, J Guo, E Gill - Acta Astronautica, 2020 - Elsevier
This paper presents innovative approaches for guidance of spacecraft formations during
reconfiguration, developed under the paradigms of cluster autonomy and safe …

Spacecraft formation flight on quasi-periodic invariant tori

N Baresi - 2017 - search.proquest.com
Since the successful rendezvous of the Gemini VI and VII spacecraft in 1965, spacecraft
formation flying has attracted the interest of many researchers in the field. Yet, existing …

Design of bounded relative trajectories in the earth zonal problem

N Baresi, DJ Scheeres - Journal of Guidance, Control, and Dynamics, 2017 - arc.aiaa.org
Numerical methods have proven to be reliable tools in generating long-term bounded
relative trajectories in nontrivial dynamical environments. Yet, none of the existing …

Bounded relative orbits in the zonal problem via high-order Poincaré maps

Y He, R Armellin, M Xu - Journal of Guidance, Control, and Dynamics, 2019 - arc.aiaa.org
Searching for naturally bounded relative orbits in a zonal gravitational field is a crucial and
challenging task in astrodynamics. In this work, a semi-analytical approach based on high …

Expansion maps: Designing relative trajectories on quasi-periodic orbits

DB Henry, DJ Scheeres - Journal of Guidance, Control, and Dynamics, 2021 - arc.aiaa.org
This work establishes a general-purpose method for designing passive spacecraft
formations by characterizing the vehicles' motion on quasi-periodic tori. First, a torus-centric …

Long-term effects of main-body's obliquity on satellite formation perturbed by third-body gravity in elliptical and inclined orbit

M Bakhtiari, K Daneshjou… - Research in Astronomy …, 2017 - iopscience.iop.org
A new non-simplified model of formation flying is derived in the presence of an oblate main-
body and third-body perturbation. In the proposed model, considering the perturbation of the …

Invariant relative orbits for spacecraft formation flying in high-order gravitational field

Y Ma, Y He, M Xu, Q Zhou, X Chen - Acta Astronautica, 2021 - Elsevier
abstract This study addresses the boundary and fluctuation of invariant relative orbits for
spacecraft formation flying in a high-order gravitational field. The invariant relative condition …

Bounded lunar relative orbits

T Nie, P Gurfil, S Zhang - Acta Astronautica, 2019 - Elsevier
Finding relative orbits for satellite formations flying around the Earth, which are long-term
bounded under various perturbations, has been a vibrant field of study. However, much less …

Spacecraft Trajectory Design and Control Leveraging Quasi-periodic Orbits

DB Henry - 2024 - search.proquest.com
Periodic orbits are the most commonly exploited dynamical structure in the preliminary
spacecraft trajectory design stages. Recent advancements now enable the efficient …

Bounded relative orbits in the zonal gravitational field for formation flying

Y He, M Xu - Journal of Guidance, Control, and Dynamics, 2018 - arc.aiaa.org
IN RECENT years the studies on distributing the functionality of large spacecraft into a group
of smaller and cooperating ones keep constantly emerging due to its successful application …