Projecte llegit
Títol: Improvement of AOCS for nanaosatellite
Estudiants que han llegit aquest projecte:
- ORTEGA COLLADO, ULISES (data lectura: 13-09-2022)
- Cerca aquest projecte a Bibliotècnica
- ORTEGA COLLADO, ULISES (data lectura: 13-09-2022)
- Cerca aquest projecte a Bibliotècnica
Director/a: PARK, HYUK
Departament: FIS
Títol: Improvement of AOCS for nanaosatellite
Data inici oferta: 18-02-2022 Data finalització oferta: 18-10-2022
Estudis d'assignació del projecte:
- DG ENG AERO/SIS TEL
Tipus: Individual | |
Lloc de realització: EETAC | |
Nom del segon director/a (UPC): David Llaveria | |
Departament 2n director/a: | |
Paraules clau: | |
Nanosatellite, testing, tracking, C++, Helmholtz coils,Image processing, GUI, ADCS, angular velocities, | |
Descripció del contingut i pla d'activitats: | |
1. Take part of the different test involving helmholtz coil.
2. Increase functionalities in the current software: 2.1. Fix Arduino - MATLAB serial communication errors for example. 2.1.Orbital representation of the simulated satelite positions 3. Change language Code in order to increase visual capabilities. For instance Go (language not decided yet). 4. Study, design and implementation of an angular speed sensor in order to be able to measure the angular speed of the platform inside the helmholtz coils.(To decide if vídeo sensor or photodiode sensor or both if posible for backup). |
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Overview (resum en anglès): | |
This work contains the analysis and improvements regarding attitude nanosatellite testing procedures. An utterly new system for measuring angular velocities has been designed from scratch in order to be applied to Cubesat testing campaigns. This system will help to track the rotations of the nanosatellite in the different tests. Knowing the angular velocity of the nanosatellite while performing the tests is so important. It allows to calibrate the gyroscopes as well as set a perfect and knows conditions to the satellite. Also, the measurements can be compared with the gyroscope angular velocityes obtained in order to recalibrate the system if necesary. Furthermore, a new design for Helmholtz coils software has been proposed using a user Interface in C++. This new software allows the user to initialize the coils with the desired magnetic fields required for testing. Two main operating ways has been considered: Static and Dynamic orbit magnetic field generation. Both systems can work altogether in order to check the attitude determination and control of the nanosatellite during testing campaigns. Nanosatellite needs to perform testing before its launch. Thus, the whole project avoids expensive risks which could doom the mission. The results obtained in this work show that the angular tracking works as desired for the testing purposes and the Helmholtz coils GUI simplifies a lot the testing process from the user point of view. |