Satellite Attitude Control System Design Taking into Account the Fuel Slosh and Flexible Dynamics
Author:
Affiliation:
1. National Institute for Space Research (INPE), Avenida dos Astronautas 1758, 12227-010 São José dos Campos, SP, Brazil
2. Brasília University, Campus Gama, Área Especial de Indústria-A-UnB, 72444-240 Brasilia, DF, Brazil
Abstract
Publisher
Hindawi Limited
Subject
General Engineering,General Mathematics
Link
http://downloads.hindawi.com/journals/mpe/2014/820586.pdf
Reference10 articles.
1. Control of Spin-Stabilized Spacecraft With Sloshing Fluid Stores
2. Dynamic coupling of a liquid-tank system under transient excitations
3. Dynamic characteristics of liquid motion in partially filled tanks of a spinning spacecraft
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