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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    Titel :

    End-to-End Mission Design & Trajectory Optimization


    Beteiligte:
    Jacob Williams (Autor:in) / Daniel A Matz (Autor:in)

    Kongress:

    Innovation Showcase Poster Session ; 2023 ; Houston, TX, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





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    Jacob Williams / Daniel Matz | NTRS


    Reentry Trajectory Optimization for Mission Analysis

    Palumbo, Roberto / Morani, Gianfranco / Cicala, Marco | AIAA | 2016


    Genesis extended mission trajectory design

    Wilson, Roby S. | NTRS | 2005


    Reentry Trajectory Optimization for Mission Analysis

    Palumbo, Roberto | Online Contents | 2017