Preliminary mission analysis GTO → asteroid 101955 Bennu in MATLAB and Python: launch window, heliocentric trajectory optimization (fmincon, ga, MultiStart / SciPy), patched conics. Cross-validated, with automated tests.
python optimization numpy matlab astrodynamics scipy matplotlib asteroid trajectory-optimization orbital-mechanics mission-analysis aerospace-engineering patched-conics space-mission-design osiris-rex bennu
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Updated
Oct 24, 2026 - Python