In-plane formation reconfiguration with radial maneuvers

Journal Article (2020)
Author(s)

Yeerang Lim (Technical University of Berlin)

Sung Hoon Mok (TU Delft - Aerospace Engineering)

Research Group
Space Systems Egineering
DOI related publication
https://doi.org/10.2514/1.G004933 Final published version
More Info
expand_more
Publication Year
2020
Language
English
Research Group
Space Systems Egineering
Issue number
10
Volume number
43
Pages (from-to)
1881-1892
Downloads counter
247
Collections
Institutional Repository
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

Formation reconfiguration with impulsive maneuvers has been continuously addressed in recent decades. The studies mostly focused on in-plane formation reconfiguration since the out-of-plane motion is independently controlled by a single burn. Most in-plane reconfiguration studies, meanwhile, rely on tangential maneuvers because of fuel efficiency and controllability of the orbital energy, compared to radial maneuvers. In this paper, the perspective differs that little influence of the radial maneuvers on the orbital energy is considered as a benefit rather than a drawback. By employing radial burns only, an effect of the thrust errors on the semimajor axis control error can be minimized. Both numerical simulations and sensitivity analysis demonstrate the robustness of the proposed radial impulsive burns compared to the conventional tangential impulsive control schemes.

Files

1.g004933.pdf
(pdf | 1.31 Mb)
License info not available