NASA NTRS · 20230014464
End-to-End Mission Design & Trajectory Optimization
Abstract
The ability to compute end-to-end mission optimized trajectories is a critical component needed for the next generation of complex human spaceflight design and operations (Orion, HLS, Gateway, Mars). This project created a new interface for two of NASA’s trajectory tools: Copernicus and Genesis, enabling them to be used together for end-to-end mission design and optimization of all flight phases, including Earth ascent, lunar ascent, rendezvous, and lunar descent. This capability can also serve as a pathfinder for developing a future autonomous, onboard trajectory optimizer.
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Jacob Williams, Daniel A Matz. End-to-End Mission Design & Trajectory Optimization. https://ntrs.nasa.gov/citations/20230014464
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