Projecte matriculat
Títol: Design of a femto-satellite for thermospheric density modeling
Director/a: GUTIÉRREZ CABELLO, JORDI
Departament: FIS
Títol: Design of a femto-satellite for thermospheric density modeling
Data inici oferta: 05-02-2026 Data finalització oferta: 05-10-2026
Estudis d'assignació del projecte:
DG ENG AERO/SIS TEL
| Tipus: Individual | |
| Lloc de realització: EETAC | |
| Segon director/a (UPC): GIL PONS, PILAR | |
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| The lower thermosphere is a critical environment for Low Earth Orbit (LEO) satellites influencing orbital lifetimes and reentry trajectories. However, this layer is highly volatile, changing based on unpredictable solar activity. Consequently, current models do not correctly predict the exact air density in real-time, thus generating uncertainties in drag estimation and orbital prediction.
This project aims to design a femto-satellite dedicated to analysing these thermospheric effects. To perform that task, a swarm of femto-satellites will be deployed to measure the atmosphere's effects on it. The core methodology involves the use of high-precision accelerometers to measure the satellite's deceleration profile. By analysing said data, the project aims to calculate the density of the atmosphere, thereby modelling the thermosphere. During this Bachelor's Thesis, the student will find suitable candidate devices: 1. Onboard computer 2. SD memory card 3. IoT transmitter 4. Antennas 5. Secondary battery 6. Solar cells 7. MEMS GNSS receiver (COCOM-free) 8. MEMS 3-axis magnetometer 9. MEMS high-accuracy accelerometer The student will propose a suitable femtosatellite architecture combining the aforementioned devices. |
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