Study and design of the attitude control of a cubesat 1U based on reaction wheels
View/Open
Memòria (amb dades confidencials) (5,793Mb) (Restricted access)
Cita com:
hdl:2117/185164
Author's e-mailpaula.sorollagmail.com
Document typeBachelor thesis
Date2019-09-30
Rights accessOpen Access
All rights reserved. This work is protected by the corresponding intellectual and industrial
property rights. Without prejudice to any existing legal exemptions, reproduction, distribution, public
communication or transformation of this work are prohibited without permission of the copyright holder
Abstract
On this thesis, the study and design of the attitude control of a cubesat 1U is performed.The mechanical model definition and the space environment description are used to develop a Simulink model where reaction wheels are used as actuators for the Attitude Control.Once the model is defined, a control algorithm taking into account external disturbances has been defined and simulated for different actuator configurations.
SubjectsArtificial satellites--Attitude control systems, Satèl·lits artificials -- Sistemes de control d'actitud
DegreeGRAU EN ENGINYERIA EN TECNOLOGIES AEROESPACIALS (Pla 2010)
Files | Description | Size | Format | View |
---|---|---|---|---|
TFG_report_PSorolla_fitxer de consulta.pdf | Memòria | 5,799Mb | View/Open | |
TFG_budget_PSorolla.pdf | Pressupost | 151,1Kb | View/Open | |
TFG_report_PSorolla.pdf | Memòria (amb dades confidencials) | 5,793Mb | Restricted access |