In-plane formation reconfiguration with radial maneuvers

Journal Article (2020)
Author(s)

Yeerang Lim (Technical University of Berlin)

S. H. Mok (TU Delft - Space Systems Egineering)

Research Group
Space Systems Egineering
Copyright
© 2020 Yeerang Lim, S. Mok
DOI related publication
https://doi.org/10.2514/1.G004933
More Info
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Publication Year
2020
Language
English
Copyright
© 2020 Yeerang Lim, S. Mok
Research Group
Space Systems Egineering
Issue number
10
Volume number
43
Pages (from-to)
1881-1892
Reuse Rights

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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.

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