Comprehensive survey and assessment of spacecraft relative motion dynamics models

J Sullivan, S Grimberg, S D'Amico - Journal of Guidance, Control, and …, 2017 - arc.aiaa.org
IN THE framework of spacecraft relative motion, current dynamics models are diverse and
often subject to a multitude of constraints and limitations on the intersatellite range of …

Survey on guidance navigation and control requirements for spacecraft formation-flying missions

G Di Mauro, M Lawn, R Bevilacqua - Journal of Guidance, Control, and …, 2018 - arc.aiaa.org
FORMATION flying (FF) has received much attention recently because of the advantages it
offers in terms of mission cost, performance, and flexibility as compared with a monolithic …

New closed-form solutions for optimal impulsive control of spacecraft relative motion

M Chernick, S D'Amico - Journal of Guidance, Control, and Dynamics, 2018 - arc.aiaa.org
This paper addresses energy-optimal guidance and control of satellite relative motion for
formation flying and rendezvous using impulsive maneuvers. To meet the requirements of …

Formation flying orbit and control concept for the visors mission

A Koenig, S D'Amico, EG Lightsey - AIAA Scitech 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-0423. vid The VIrtual Super Optics
Reconfigurable Swarm (VISORS) mission is a distributed telescope consisting of two 6U …

[PDF][PDF] Long-term analytical propagation of satellite relative motion in perturbed orbits

T Guffanti, S D'Amico… - 27th AAS/AIAA Space …, 2017 - slab.sites.stanford.edu
Many scientific applications require the implementation of satellite formation-flying in various
orbits both around Earth and other planetary bodies. The design and guidance of these new …

Continuous maneuvers for spacecraft formation flying reconfiguration using relative orbit elements

G Di Mauro, R Bevilacqua, D Spiller, J Sullivan… - Acta Astronautica, 2018 - Elsevier
This paper presents the solutions to the spacecraft relative trajectory reconfiguration
problem when a continuous thrust profile is used, and the reference orbit is circular. Given a …

An Interpolated Second-Order Relative Motion Model for Gateway

D Cunningham, RP Russell - The Journal of the Astronautical Sciences, 2023 - Springer
Understanding of relative motion dynamics is essential for many spaceflight objectives, from
orbit determination to rendezvous. Although these dynamics are well understood in a …

[PDF][PDF] Angles-only navigation for autonomous on-orbit space situational awareness applications

J Sullivan, TA Lovell, S D'Amico - AAS/AIAA Astrodynamics …, 2018 - slab.sites.stanford.edu
This paper addresses the design and validation of a prototype angles-only estimation
architecture for on-orbit space situational awareness applications. The proposed navigation …

Observability analysis and optimization for angles-only navigation of distributed space systems

J Kruger, S D'Amico - Advances in Space Research, 2024 - Elsevier
Angles-only navigation methods are compelling for distributed space systems (DSS) such as
swarms and constellations. However, complex dependencies between state observability …

Output regulation control for satellite formation flying using differential drag

M Shouman, M Bando, S Hokamoto - Journal of guidance, control, and …, 2019 - arc.aiaa.org
This paper proposes a new approach of using differentials in aerodynamic drag in
combination with thrusters to control satellite formation flying in low Earth orbits …