This paper presents a three-dimensional model for maneuvering of a spacecraft with unactuated fuel slosh dynamics, and uses Lagrangian for multi-pendulum analogy to obtain a mathematical model. Using of multi-pendulum model could be the best way for characterize the most fluid sloshing modes. Also, whole the fuel in the container is modeled by a fixed mass and two sloshing masses.


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    Title :

    3D multi-pendulum model of slosh dynamics in a spacecraft


    Contributors:
    Navabi, M. (author) / Davoodi, Ali (author)


    Publication date :

    2017-06-01


    Size :

    423725 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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