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Multi-criteria and multi-objective dynamic planning by self-adaptive multi-agent system, application to earth observation satellite constellations

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Academic year: 2021

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Figure

Figure 1.1 — Mission chain and operational concepts
Figure 1.6 — Difference between agile and non-agile satellite
Figure 1.9 represents an orbit around the Earth and the three orbital parameter (inclination i, the longitude of ascending node Ω and the argument of periapsis ω useful to determine a position on the orbit).
Table 2.2 — Exact methods synthesis
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