R Kristiansen, PJ Nicklasson - Acta Astronautica, 2009 - Elsevier
This paper presents a review of previous work within the field of spacecraft formation flying, including modeling approaches and controller design. In addition, five new approaches for …
Analytical Mechanics of Space Systems by Hanspeter Schaub and John Junkins is a comprehensive treatment of a stimulating and challenging subject that is both old and new …
DP Scharf, FY Hadaegh… - Proceedings of the 2004 …, 2004 - ieeexplore.ieee.org
Formation flying is defined as a set of more than one spacecraft whose states are coupled through a common control law. This paper provides a comprehensive survey of spacecraft …
HS Ahn, KL Moore, YQ Chen - International Journal of Robust …, 2010 - Wiley Online Library
This paper proposes an iterative learning control (ILC) scheme to ensure trajectory‐keeping in satellite formation flying. Since satellites rotate the earth periodically, position‐dependent …
M Pontani, M Pustorino - Acta Astronautica, 2021 - Elsevier
This research is focused on the definition, analysis, and numerical testing of an effective nonlinear orbit control technique tailored to compensating orbit perturbations, as well as …
S Silvestrini, M Lavagna - Advances in Space Research, 2021 - Elsevier
This paper presents a neural-aided Guidance, Navigation & Control algorithm for reconfiguration of distributed space systems. The guidance algorithm is based on Artificial …
This survey deals with the problem of the group motion of spacecraft, which is rapidly developing and relevant for many applications, in terms of developing the onboard control …
AW Koenig, B Macintosh, S D'Amico - Journal of Spacecraft and …, 2019 - arc.aiaa.org
This paper presents a new formation design that enables deployment of large distributed telescopes aligned with inertial targets in Earth orbit. To minimize propellant consumption …
AD Ogundele - Aerospace Science and Technology, 2021 - Elsevier
Generally, spacecraft relative orbit is described using Hill frame coordinates with which it is difficult to obtain precise orbit geometry. The orbit description is made simpler and …