ASTRA CanSat Final Design Review — Cansats in Poland Competition
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| Natura: | Recurso digital |
| Lingua: | inglese |
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Zenodo
2026
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| _version_ | 1866901715463176192 |
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| author | Stuczyński, Wojciech Dąbrowski, Bartosz Wójcik, Antoni Pupek, Dawid Jakub, Wąsikowski Nowakowska, Pola |
| author_facet | Stuczyński, Wojciech Dąbrowski, Bartosz Wójcik, Antoni Pupek, Dawid Jakub, Wąsikowski Nowakowska, Pola |
| contents | <p class="font-claude-response-body break-words whitespace-normal leading-[1.7]">This document is the Final Design Review (FDR) report of Team ASTRA from Poland, prepared for the Cansats in Europe competition organized by the European Space Agency (ESA). The report presents the complete design of a CanSat probe that functions as a compact, foldable quadcopter drone capable of fitting within standard CanSat dimensional constraints (66 mm diameter, 114 mm height).</p> <p class="font-claude-response-body break-words whitespace-normal leading-[1.7]">The primary mission involves measuring temperature and pressure during descent from approximately 2500 meters, transmitting telemetry data via LoRa (433 MHz) to a custom-built ground station. The secondary mission, inspired by NASA's Ingenuity Mars Helicopter, focuses on autonomous terrain surveying — the probe deploys folding arms mid-flight, detaches its parachute using a thermal release system, and conducts a photogrammetric scan of a 250 m × 250 m area at 15 meters altitude. The captured images are processed using Autodesk ReCap Pro to generate 3D terrain models and contour maps.</p> <p class="font-claude-response-body break-words whitespace-normal leading-[1.7]">The report covers mechanical and structural design, electrical schematics, PCB design, software architecture (Arduino-based primary mission control and ArduPilot-based flight control), recovery systems, ground support equipment, power budget and flight time calculations, test campaign results, safety measures, project planning, budget, and the team's outreach programme. All team members hold A1/A3 drone pilot certificates.</p> <p class="font-claude-response-body break-words whitespace-normal leading-[1.7]">Total mass: 348.6 g. Estimated flight time: 25.6 minutes. Total project cost: 521.72 EUR.</p> |
| format | Recurso digital |
| id | zenodo_https___doi_org_10_5281_zenodo_19542759 |
| institution | Zenodo |
| language | eng |
| publishDate | 2026 |
| publisher | Zenodo |
| record_format | zenodo |
| spellingShingle | ASTRA CanSat Final Design Review — Cansats in Poland Competition Stuczyński, Wojciech Dąbrowski, Bartosz Wójcik, Antoni Pupek, Dawid Jakub, Wąsikowski Nowakowska, Pola CanSat Drone photogrammetry terrain mapping ESA student project <p class="font-claude-response-body break-words whitespace-normal leading-[1.7]">This document is the Final Design Review (FDR) report of Team ASTRA from Poland, prepared for the Cansats in Europe competition organized by the European Space Agency (ESA). The report presents the complete design of a CanSat probe that functions as a compact, foldable quadcopter drone capable of fitting within standard CanSat dimensional constraints (66 mm diameter, 114 mm height).</p> <p class="font-claude-response-body break-words whitespace-normal leading-[1.7]">The primary mission involves measuring temperature and pressure during descent from approximately 2500 meters, transmitting telemetry data via LoRa (433 MHz) to a custom-built ground station. The secondary mission, inspired by NASA's Ingenuity Mars Helicopter, focuses on autonomous terrain surveying — the probe deploys folding arms mid-flight, detaches its parachute using a thermal release system, and conducts a photogrammetric scan of a 250 m × 250 m area at 15 meters altitude. The captured images are processed using Autodesk ReCap Pro to generate 3D terrain models and contour maps.</p> <p class="font-claude-response-body break-words whitespace-normal leading-[1.7]">The report covers mechanical and structural design, electrical schematics, PCB design, software architecture (Arduino-based primary mission control and ArduPilot-based flight control), recovery systems, ground support equipment, power budget and flight time calculations, test campaign results, safety measures, project planning, budget, and the team's outreach programme. All team members hold A1/A3 drone pilot certificates.</p> <p class="font-claude-response-body break-words whitespace-normal leading-[1.7]">Total mass: 348.6 g. Estimated flight time: 25.6 minutes. Total project cost: 521.72 EUR.</p> |
| title | ASTRA CanSat Final Design Review — Cansats in Poland Competition |
| topic | CanSat Drone photogrammetry terrain mapping ESA student project |
| url | https://doi.org/10.5281/zenodo.19542759 |