Numerical integration for continuously thrusting spacecraft optimal trajectory, considering rectangular Cartesian and polar cylindrical coordinates characteristics


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Coordinate system influence on the regularized trajectory optimization problem.


    Contributors:

    Conference:

    ASTRODYNAMICS CONFERENCE ; 1969 ; PRINCETON, NJ


    Publication date :

    1969-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :