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.
3D multi-pendulum model of slosh dynamics in a spacecraft
2017-06-01
423725 byte
Conference paper
Electronic Resource
English
AIAA-2005-2751 Modeling Spacecraft Fuel Slosh Using Pendulum Analogs
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