Space Science and Technology

Space subsystems design: (navigation, control, structure and…)

Stability Analysis and Nonlinear Modeling of Coupled Slosh-Tank Dynamics: Analytical Equivalent Pendulum Approach

Milad َAzimi

Articles in Press, Accepted Manuscript, Available Online from 07 April 2022

Abstract

This paper deals with semi-analytical modeling and stability analysis of a coupled slosh-tank dynamics as a multibody system using the Homotopy Perturbation Method (HPM). The sloshing motion of the liquid inside the tank is considered as the equivalent pendulum model. The nonlinear equations of the motion ... Read More

View Article

Modeling and Control of Fuel Sloshing and its Effect on Spacecraft Attitude

M. Navabi; A. Davodi

Volume 11, Issue 4 , December 2018, , Pages 11-22

Abstract

Sloshing phenomenon in spacecraft fuel tank during orbital maneuver, causes adverse effects on spacecraft attitude. Therefore, before orbital maneuvers, modeling fuel sloshing and determining appropriate method for controlling it has to be carried out. The aim of this paper is to model slosh dynamics ... Read More

Space Science and Technology

Articles in Press

Current Issue

Volume 17 (2024)

Volume 16 (2023)

Volume 15 (2022)

Volume 14 (2021)

Volume 13 (2020)

Volume 12 (2019)

Volume 11 (2018)

Volume 10 (2017)

Volume 9 (2016)

Volume 8 (2015)

Volume 7 (2014)

Volume 6 (2013)

Volume 5 (2012)

Volume 4 (2011)

Volume 3 (2010)

Volume 2 (2009)

Volume 1 (2008)

Keywords = Sloshing

Stability Analysis and Nonlinear Modeling of Coupled Slosh-Tank Dynamics: Analytical Equivalent Pendulum Approach

Abstract

Modeling and Control of Fuel Sloshing and its Effect on Spacecraft Attitude

Abstract