Abstract
This paper presents the qualification of affordable, open-source analog (PSS) and digital Sun sensors (DSS) for CubeSats, which aim to provide cost-effective and accessible attitude determination solutions for small satellite missions. The study evaluates the performance, reliability, and suitability of these sensors in space-like conditions, addressing key factors such as accuracy, thermal stability, and radiation tolerance. Experimental results demonstrate that the PSS can achieve better than 5° precision over a field of view of 100° while maintaining low costs and power consumption. The DSS shows a precision better than 0.5° over a field of view of 36° using a photolithographically patterned optical aperture acting as a pinhole. The research highlights the potential of these sensors to democratize access to space technology, supporting academic and commercial CubeSat missions with accessible and effective attitude determination solutions.
| Original language | English |
|---|---|
| Pages (from-to) | 7352-7372 |
| Number of pages | 21 |
| Journal | Advances in Space Research |
| Volume | 77 |
| Issue number | 6 |
| DOIs | |
| Publication status | Published - 2026 |
| MoE publication type | A1 Journal article-refereed |
Funding
The following work was performed as part of and financed by the Finnish Centre of Excellence in Research of Sustainable Space (FORESAIL), which is a project under the Research Council of Finland decision numbers 336805 to 336809.
Keywords
- CubeSat
- Qualification
- Radiation
- Sun sensors
- Testing
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