A paper describes algorithms for guidance and control (G&C) of a spacecraft maneuvering near a planet, moon, asteroid, comet, or other small astronomical body. The algorithms were developed following a model-predictive-control approach along with a convexification of the governing dynamical equations, control constraints, and trajectory and state constraints.


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    Title :

    Pseudo-Waypoint Guidance for Proximity Spacecraft Maneuvers


    Contributors:


    Publication date :

    2007-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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