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An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites
The High Energy Rapid Modular Ensemble of Satellites (HERMES) is a constellation of 3U nano-satellites for high energy astrophysics. The HERMES nano-satellites’ components have been designed, verified, and tested to detect and localize energetic astrophysical transients, such as short gamma-ray burs...
Autores principales: | , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
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MDPI
2023
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10007507/ https://www.ncbi.nlm.nih.gov/pubmed/36904596 http://dx.doi.org/10.3390/s23052393 |
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author | Colagrossi, Andrea Lavagna, Michèle Bertacin, Roberto |
author_facet | Colagrossi, Andrea Lavagna, Michèle Bertacin, Roberto |
author_sort | Colagrossi, Andrea |
collection | PubMed |
description | The High Energy Rapid Modular Ensemble of Satellites (HERMES) is a constellation of 3U nano-satellites for high energy astrophysics. The HERMES nano-satellites’ components have been designed, verified, and tested to detect and localize energetic astrophysical transients, such as short gamma-ray bursts (GRBs), which are the electromagnetic counterparts of gravitational wave events, thanks to novel miniaturized detectors sensitive to X-rays and gamma-rays. The space segment is composed of a constellation of CubeSats in low-Earth orbit (LEO), ensuring an accurate transient localization in a field of view of several steradians exploiting the triangulation technique. To achieve this goal, guaranteeing a solid support to future multi-messenger astrophysics, HERMES shall determine its attitude and orbital states with stringent requirements. The scientific measurements bind the attitude knowledge within 1 deg ([Formula: see text]) and the orbital position knowledge within 10 m ([Formula: see text]). These performances shall be reached considering the mass, volume, power, and computation constraints of a 3U nano-satellite platform. Thus, an effective sensor architecture for full-attitude determination was developed for the HERMES nano-satellites. The paper describes the hardware typologies and specifications, the configuration on the spacecraft, and the software elements to process the sensors’ data to estimate the full-attitude and orbital states in such a complex nano-satellite mission. The aim of this study was to fully characterize the proposed sensor architecture, highlighting the available attitude and orbit determination performance and discussing the calibration and determination functions to be implemented on-board. The presented results derived from model-in-the-loop (MIL) and hardware-in-the-loop (HIL) verification and testing activities and can serve as useful resources and a benchmark for future nano-satellite missions. |
format | Online Article Text |
id | pubmed-10007507 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2023 |
publisher | MDPI |
record_format | MEDLINE/PubMed |
spelling | pubmed-100075072023-03-12 An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites Colagrossi, Andrea Lavagna, Michèle Bertacin, Roberto Sensors (Basel) Article The High Energy Rapid Modular Ensemble of Satellites (HERMES) is a constellation of 3U nano-satellites for high energy astrophysics. The HERMES nano-satellites’ components have been designed, verified, and tested to detect and localize energetic astrophysical transients, such as short gamma-ray bursts (GRBs), which are the electromagnetic counterparts of gravitational wave events, thanks to novel miniaturized detectors sensitive to X-rays and gamma-rays. The space segment is composed of a constellation of CubeSats in low-Earth orbit (LEO), ensuring an accurate transient localization in a field of view of several steradians exploiting the triangulation technique. To achieve this goal, guaranteeing a solid support to future multi-messenger astrophysics, HERMES shall determine its attitude and orbital states with stringent requirements. The scientific measurements bind the attitude knowledge within 1 deg ([Formula: see text]) and the orbital position knowledge within 10 m ([Formula: see text]). These performances shall be reached considering the mass, volume, power, and computation constraints of a 3U nano-satellite platform. Thus, an effective sensor architecture for full-attitude determination was developed for the HERMES nano-satellites. The paper describes the hardware typologies and specifications, the configuration on the spacecraft, and the software elements to process the sensors’ data to estimate the full-attitude and orbital states in such a complex nano-satellite mission. The aim of this study was to fully characterize the proposed sensor architecture, highlighting the available attitude and orbit determination performance and discussing the calibration and determination functions to be implemented on-board. The presented results derived from model-in-the-loop (MIL) and hardware-in-the-loop (HIL) verification and testing activities and can serve as useful resources and a benchmark for future nano-satellite missions. MDPI 2023-02-21 /pmc/articles/PMC10007507/ /pubmed/36904596 http://dx.doi.org/10.3390/s23052393 Text en © 2023 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 Colagrossi, Andrea Lavagna, Michèle Bertacin, Roberto An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites |
title | An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites |
title_full | An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites |
title_fullStr | An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites |
title_full_unstemmed | An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites |
title_short | An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites |
title_sort | effective sensor architecture for full-attitude determination in the hermes nano-satellites |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10007507/ https://www.ncbi.nlm.nih.gov/pubmed/36904596 http://dx.doi.org/10.3390/s23052393 |
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