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http://dx.doi.org/10.5139/JKSAS.2017.45.12.1059

Analysis of Spacecraft Attitude Dynamics Interacting with Liquid Fuel Sloshing  

Jin, Jaehyun (Dept. Aerospace Eng./Center for Aerospace Eng. Research, Sunchon National University)
Kim, Su-Kyum (Satellite Mechanical Team, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.45, no.12, 2017 , pp. 1059-1068 More about this Journal
Abstract
Space exploration spacecraft carry large amounts of liquid fuel, often more than half. In such cases, the liquid fuel sloshing must be considered in the design of the spacecraft since the sloshing can affects the stability of the spacecraft. In this paper, we present the results of analyzing the sloshing of fuel and the dynamic behavior of the spacecraft. For the purpose, a model in which the maneuvering of the spacecraft causes the sloshing and a model in which the reaction force and moment due to the sloshing are transmitted to the spacecraft are developed. The dynamical behavior of the spacecraft are analyzed using a simulation program coded by Modelica.
Keywords
Spacecraft Dynamics; Liquid Sloshing; Spherical Pendulum Model; Modelica Program;
Citations & Related Records
Times Cited By KSCI : 4  (Citation Analysis)
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