A semi-analytical method for periodic earth coverage satellites optimization
In this paper, we address a problem of designing satellite constellations to deal with a sequence of Earth revisit missions in the presence of limited resource capabilities. In order to fulfill the periodic coverage requirements, we take the repeating ground-track orbit into account and propose a se...
Gespeichert in:
| Hauptverfasser: | , |
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| Dokumenttyp: | Article (Journal) |
| Sprache: | Englisch |
| Veröffentlicht: |
[March 2018]
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| In: |
IEEE communications letters
Year: 2017, Jahrgang: 22, Heft: 3, Pages: 534-537 |
| ISSN: | 1089-7798 |
| DOI: | 10.1109/LCOMM.2017.2780107 |
| Online-Zugang: | Verlag, Volltext: https://doi.org/10.1109/LCOMM.2017.2780107
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| Verfasserangaben: | Xiaoyu Chen , Guangming Dai, Gerhard Reinelt, and Maocai Wang |
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| 245 | 1 | 2 | |a A semi-analytical method for periodic earth coverage satellites optimization |c Xiaoyu Chen , Guangming Dai, Gerhard Reinelt, and Maocai Wang |
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| 520 | |a In this paper, we address a problem of designing satellite constellations to deal with a sequence of Earth revisit missions in the presence of limited resource capabilities. In order to fulfill the periodic coverage requirements, we take the repeating ground-track orbit into account and propose a semi-analytical method. After analyzing the coverage capacity of the resource for a random spot target on Earth's surface, we define and calculate the feasible longitude interval of ascending node of the orbit. Subsequently, a mixed integer linear programming (MILP) model and an improved 0/1 programming model are formulated with coverage constraints that considerably reduce the size of the search space. We demonstrate that the new method significantly improves the optimization efficiency and verify the robustness of the solution. | ||
| 534 | |c 2017 | ||
| 650 | 4 | |a ascending node | |
| 650 | 4 | |a Computational modeling | |
| 650 | 4 | |a constellation design | |
| 650 | 4 | |a coverage analysis | |
| 650 | 4 | |a coverage capacity | |
| 650 | 4 | |a coverage constraints | |
| 650 | 4 | |a Earth | |
| 650 | 4 | |a Earth revisit mission sequence | |
| 650 | 4 | |a Earth surface | |
| 650 | 4 | |a Harmonic analysis | |
| 650 | 4 | |a improved 0/1 programming model | |
| 650 | 4 | |a integer programming | |
| 650 | 4 | |a limited resource capabilities | |
| 650 | 4 | |a linear programming | |
| 650 | 4 | |a MILP model | |
| 650 | 4 | |a mixed integer linear programming model | |
| 650 | 4 | |a modelling | |
| 650 | 4 | |a optimization | |
| 650 | 4 | |a optimization efficiency | |
| 650 | 4 | |a periodic coverage requirements | |
| 650 | 4 | |a periodic Earth coverage satellites optimization | |
| 650 | 4 | |a Planetary orbits | |
| 650 | 4 | |a random spot target | |
| 650 | 4 | |a repeating ground-track orbit | |
| 650 | 4 | |a satellite communication | |
| 650 | 4 | |a Satellite communication | |
| 650 | 4 | |a satellite constellations | |
| 650 | 4 | |a Satellite constellations | |
| 650 | 4 | |a Satellites | |
| 650 | 4 | |a search problems | |
| 650 | 4 | |a search space size | |
| 650 | 4 | |a semianalytical method | |
| 700 | 1 | |a Reinelt, Gerhard |e VerfasserIn |0 (DE-588)101987113X |0 (DE-627)691042861 |0 (DE-576)358936187 |4 aut | |
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