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End-to-End Mission Design & Trajectory OptimizationThe 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.
Document ID
20230014464
Acquisition Source
Johnson Space Center
Document Type
Poster
Authors
Jacob Williams
(Johnson Space Center Houston, Texas, United States)
Daniel A Matz
(Johnson Space Center Houston, Texas, United States)
Date Acquired
October 4, 2023
Subject Category
Astrodynamics
Meeting Information
Meeting: Innovation Showcase Poster Session
Location: Houston, TX
Country: US
Start Date: December 1, 2023
End Date: December 2, 2023
Sponsors: Johnson Space Center
Funding Number(s)
WBS: 573754.01.01.01.18.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Software
Trajectory Design
Optimization
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