The fundamental methods are described for the general spacecraft trajectory design and optimization software system called Copernicus. The methods rely on a unified framework that is used to model, design, and optimize spacecraft trajectories that may operate in complex gravitational force fields, use multiple propulsion systems, and involve multiple spacecraft. The trajectory model, with its associated equations of motion and maneuver models, are discussed.


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    Title :

    Theoretical Foundation of Copernicus: A Unified System for Trajectory Design and Optimization


    Contributors:

    Conference:

    4th International Conference on Astrodynamics Tools and Techniques ; 2010 ; Madrid, Spain


    Publication date :

    2010-05-03


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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