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Navigation analysis and manoeuvres design for the European Student Moon Orbiter

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Figure

Fig. 1. Perilune lifetime with 1% error in the initial orbital elements.
Fig. 2. Perilune lifetime for a 3% error in the initial orbital elements.
Fig. 4. Relative error in position (left) and velocity (right) projected along the radial, transversal and out of plane reference frame
Fig. 7. Position dispersion at 1 week from lunar injection, r-h plane.
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