Satellite Mission Analysis and Design based on Orekit
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Updated
Jun 11, 2023 - Python
Satellite Mission Analysis and Design based on Orekit
Trajectory optimization framework that uses indirect methods
Preliminary Design Of The Trajectory For An Interplanetary Mission Between Earth And Saturn With Natural Gravitatory Assistance From Jupiter
High-fidelity illumination modeling and N-body trajectory optimization for Enceladus mission design. Developed in MATLAB for the ESA-funded GIGANTES project.
Delta-v planner for circular-to-circular transfers (Hohmann, bi-elliptic, plane-change). Impulsive burns, quick trade-offs. Python 3.10+.
Aerospace Engineering Portfolio - GNC Systems, Mission Analysis, and Space Systems Design
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