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START: A Satellite Three Axis Rotation Testbed

The main goal of this paper is to illustrate the development of a satellite attitude simulator testbed for on-ground experimentation of attitude, determination, and control methodologies. This setup aims to be a low-cost alternative to testbeds based on air-bearing couplings. Our system is mainly co...

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Detalles Bibliográficos
Autores principales: Lavezzi, Giovanni, Stang, Nathan J., Ciarcià, Marco
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8879640/
https://www.ncbi.nlm.nih.gov/pubmed/35208290
http://dx.doi.org/10.3390/mi13020165
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author Lavezzi, Giovanni
Stang, Nathan J.
Ciarcià, Marco
author_facet Lavezzi, Giovanni
Stang, Nathan J.
Ciarcià, Marco
author_sort Lavezzi, Giovanni
collection PubMed
description The main goal of this paper is to illustrate the development of a satellite attitude simulator testbed for on-ground experimentation of attitude, determination, and control methodologies. This setup aims to be a low-cost alternative to testbeds based on air-bearing couplings. Our system is mainly composed of a suspended base, a single-board processor, a set of reaction wheels, and a battery. The suspension system entails a set of thin high-tensile strength wires converging on a single wire, which is in turn connected to the base. This configuration allows a three degrees-of-freedom rotation range and minimal resistive torque in all the rotations axis. The adjustability of the hanging point at the base, and a set of sliding masses, allow us to achieve a quite accurate superposition of rotation point and center of mass for a quasi-neutral equilibrium. The testbed is completed by a PC workstation, to generate and stream the desired angular rates of the wheels, and a motion capture system for attitude determination.
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spelling pubmed-88796402022-02-26 START: A Satellite Three Axis Rotation Testbed Lavezzi, Giovanni Stang, Nathan J. Ciarcià, Marco Micromachines (Basel) Article The main goal of this paper is to illustrate the development of a satellite attitude simulator testbed for on-ground experimentation of attitude, determination, and control methodologies. This setup aims to be a low-cost alternative to testbeds based on air-bearing couplings. Our system is mainly composed of a suspended base, a single-board processor, a set of reaction wheels, and a battery. The suspension system entails a set of thin high-tensile strength wires converging on a single wire, which is in turn connected to the base. This configuration allows a three degrees-of-freedom rotation range and minimal resistive torque in all the rotations axis. The adjustability of the hanging point at the base, and a set of sliding masses, allow us to achieve a quite accurate superposition of rotation point and center of mass for a quasi-neutral equilibrium. The testbed is completed by a PC workstation, to generate and stream the desired angular rates of the wheels, and a motion capture system for attitude determination. MDPI 2022-01-22 /pmc/articles/PMC8879640/ /pubmed/35208290 http://dx.doi.org/10.3390/mi13020165 Text en © 2022 by the authors. https://creativecommons.org/licenses/by/4.0/Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/).
spellingShingle Article
Lavezzi, Giovanni
Stang, Nathan J.
Ciarcià, Marco
START: A Satellite Three Axis Rotation Testbed
title START: A Satellite Three Axis Rotation Testbed
title_full START: A Satellite Three Axis Rotation Testbed
title_fullStr START: A Satellite Three Axis Rotation Testbed
title_full_unstemmed START: A Satellite Three Axis Rotation Testbed
title_short START: A Satellite Three Axis Rotation Testbed
title_sort start: a satellite three axis rotation testbed
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8879640/
https://www.ncbi.nlm.nih.gov/pubmed/35208290
http://dx.doi.org/10.3390/mi13020165
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