Optimisation of the Energy Harvesting and Management Systems of the Nanosatellite OUFTI-2 and Design of its Electrical Power Supply
Grosjean, François
Promoteur(s) : Vanderbemden, Philippe
Date de soutenance : 26-jui-2019/27-jui-2019 • URL permanente : http://hdl.handle.net/2268.2/6790
Détails
Titre : | Optimisation of the Energy Harvesting and Management Systems of the Nanosatellite OUFTI-2 and Design of its Electrical Power Supply |
Titre traduit : | [fr] Optimisation du système de gestion de l'énergie du nanosatellite OUFTI-2 et test de son alimentation électrique (EPS) |
Auteur : | Grosjean, François |
Date de soutenance : | 26-jui-2019/27-jui-2019 |
Promoteur(s) : | Vanderbemden, Philippe |
Membre(s) du jury : | Broun, Valery
Redouté, Jean-Michel Verly, Jacques |
Langue : | Anglais |
Nombre de pages : | 105 |
Mots-clés : | [en] OUFTI-2 [en] CubeSat [en] Power Budget [en] Electrical Power Supply [en] Semi-regulated Bus [en] D-STAR [en] Power Path |
Discipline(s) : | Ingénierie, informatique & technologie > Ingénierie électrique & électronique |
Public cible : | Etudiants Grand public |
Institution(s) : | Université de Liège, Liège, Belgique |
Diplôme : | Master : ingénieur civil électricien, à finalité spécialisée en "electronic systems and devices" |
Faculté : | Mémoires de la Faculté des Sciences appliquées |
Résumé
[en] The aim of this thesis is to design a part of the Electrical Power Supply (EPS) board of the nanosatellite OUFTI-2. The parameters to be fixed are the solar panels’ configuration and management, the Battery Management System (BMS), and their connection to the DC-DC converters distributing the power to all sub-systems. The battery pack, the solar panels and the DC-DC converters are already chosen from previous works on the satellite. The limitations and requirements imposed by the choice of these components are analysed. The state of the art of Maximum Power Point Tracking (MPPT)technology as well as Battery Management Systems (BMS) of Lithium-Polymer (LiPo) are summarised and compared. From this knowledge, several relevant EPS designs combining different MPPT controllers and BMS configurations are discussed and tested as well as their power paths. The final design is chosen to be a semi-regulated bus architecture connecting two SPV1040 MPPT controllers in series and an MCP73213 linear BCR to the DC-DC converters. Finally, the power budget of the satellite’s consumption and harvested power based on the chosen design is discussed. This first analysis ensures a net power margin of 300mW in the worst case orbit scenario, for a standard mode operation.
Fichier(s)
Document(s)
Description: Summary of the thesis in one page
Taille: 122.35 kB
Format: Adobe PDF
Annexe(s)
Description: Matlab script to plot several I-V curve of OUFTI-2's solar panel based on the temperature
Taille: 980 B
Format: Unknown
Description: Matlab script to plot several I-V curves of OUFTI-2's solar panel based on the insolation
Taille: 961 B
Format: Unknown
Description: Matlab script to model a 28% efficiency solar cell from Spectrolab
Taille: 1.64 kB
Format: Unknown
Description: Matlab script to plot the I-V curve of a solar panel of OUFTI-2 based on Temperature and Insolation
Taille: 838 B
Format: Unknown
Description: POSTER of my thesis for a presentation made during the SSSIF event in Malaga
Taille: 482.17 kB
Format: Adobe PDF
Description: Schematic of the battery charger block of the PCB
Taille: 90.21 kB
Format: Adobe PDF
Description: Schematic of the two SPV1040 blocks of the PCB
Taille: 84.62 kB
Format: Adobe PDF
Description: Layout of the prototype PCB to test the SPV1040 MPPT controllers
Taille: 57.54 kB
Format: Adobe PDF
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