Multi-rendezvous Spacecraft Trajectory Optimization with Beam P-ACO
Low-thrust mission design for asteroid mining and beyond: which targets a spacecraft can reach, sizing the spacecraft to get there, and planning the trajectory to fly.
An entry into to the world of spacecraft trajectory design and optimization. The problem statement is to capture two planetary systems with one launch from earth, which means the initial part of the trajectory of a spacecraft which separates into two has to be the same. After separation, one half of the spacecraft will capture Saturn after takin…
Orbital trajectory optimization: pykep/pygmo screening + tudatpy verification, CUDA-batched, with a PySide6/PyVista Mission Control 3D viewer.
🚀 Integrated differentiable trajectory optimization and economic analysis platform for LEO-Moon missions. Combines PyKEP orbital mechanics with economic modeling for mission planning.
Benchmarking Astrodynamics solutions
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