Experimental comparison of attitude controllers for nanosatellites

Bello García, Alvaro ORCID: https://orcid.org/0000-0002-2145-6344, Olfe García, Karl Stephan, Ezquerro Navarro, José Miguel ORCID: https://orcid.org/0000-0002-8863-298X, Rodriguez Otero, Jacobo ORCID: https://orcid.org/0000-0002-3561-7276 and Lapuerta Gonzalez, Maria Victoria ORCID: https://orcid.org/0000-0002-7472-797X (2019). Experimental comparison of attitude controllers for nanosatellites. In: "8th EUropean Conference for Aeronautics and Space Sciences (EUCASS)", 1-4 jul 2019, Madrid. pp. 1-15.

Description

Title: Experimental comparison of attitude controllers for nanosatellites
Author/s:
Item Type: Presentation at Congress or Conference (Article)
Event Title: 8th EUropean Conference for Aeronautics and Space Sciences (EUCASS)
Event Dates: 1-4 jul 2019
Event Location: Madrid
Title of Book: 8th European Conference for Aeronautics and Space Sciences (EUCASS 2019)
Date: 2019
Subjects:
Faculty: E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM)
Department: Aeronaves y Vehículos Espaciales
Creative Commons Licenses: Recognition - No derivative works - Non commercial

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Abstract

Nowadays, the attitude controllers based on artificial intelligence are being designed giving very good results compared with classical controllers. However, the performance comparisons made until now have been based on numerical simulations, being necessary experimental data and on-board tests. In this work, a PID and a Fuzzy-logic based controllers have been developed for an educational nanosatellite (ESAT). Through the intensive use of the ESAT we have tested and compared the performance from an experimental point of view. Four performance indexes (accuracy, cost, stability and robustness) have been used to quantify the performance of each controller.

More information

Item ID: 67220
DC Identifier: https://oa.upm.es/67220/
OAI Identifier: oai:oa.upm.es:67220
Deposited by: Memoria Investigacion
Deposited on: 16 Nov 2021 09:37
Last Modified: 16 Nov 2021 09:37
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