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Journals / Journal of Scientific Reports-C / 2026 / Sayı: 007

Design of a Model Satellite Consisting of Container and Payload for the Teknofest 2023 Competition

Teknofest 2023 Yarışması için Taşıyıcı ve Faydalı Yükten Oluşan Bir Model Uydu Tasarımı

Cemil Özgültekin(KUTAHYA DUMLUPINAR UNIVERSITY)0009-0009-5115-4740
Yasin Turanlı(KUTAHYA DUMLUPINAR UNIVERSITY)0000-0003-2316-9151
Şerif Ali Sadık(DUMLUPINAR UNIVERSITY)0000-0003-2883-1431
Pages
10–24
Publication Date
2024-08-31
DOI
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

Subsequent to hardware and mechanical development, the software development process commenced in three distinct phases: hardware integration, communication software, and ground station software, each essential for autonomous missions.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:This work presents the design of a model communication satellite featuring an autonomously separable mission mechanism.
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Key Findings & Data:The design emphasizes mobility and simplicity to meet the requirements of Teknofest model satellite competition 2023.
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Conclusion & Impact:Subsequent to hardware and mechanical development, the software development process commenced in three distinct phases: hardware integration, communication software, and ground station software, each essential for autonomous missions.
🔬Design:Modeling & Simulation
📍Scope:2023 Verileri
⚙️Variables:Model Uydu · Görev Yükü · Taşıyıcı

Abstract

This work presents the design of a model communication satellite featuring an autonomously separable mission mechanism. Focusing on originality and efficiency, the model satellite is designed in two parts: the container and the payload. The model satellite is configured with software and necessary mechanical-electronic components to gather relevant data with the sensors placed on the payload. The design emphasizes mobility and simplicity to meet the requirements of Teknofest model satellite competition 2023. The development process adhered to specific work packages, culminating in the configuration of components to meet vehicle requirements. Subsequent to hardware and mechanical development, the software development process commenced in three distinct phases: hardware integration, communication software, and ground station software, each essential for autonomous missions.

Özet

Bu çalışma, otonom olarak ayrılabilen bir görev mekanizmasına sahip model bir haberleşme uydusunun tasarımını sunmaktadır. Özgünlük ve verimliliğe odaklanan model uydu, taşıyıcı ve faydalı yük olmak üzere iki parça halinde tasarlanmıştır. Model uydu, faydalı yük üzerine yerleştirilen sensörlerle, ilgili verileri toplamak için yazılım ve gerekli mekanik-elektronik bileşenlerle yapılandırılmıştır. Tasarım, Teknofest Model Uydu Yarışması 2023'ün gerekliliklerini karşılamak için mobilite ve basitliği vurgulamaktadır. Geliştirme süreci, belirli iş paketlerine bağlı kalarak, araç gereksinimlerini karşılamak için bileşenlerin yapılandırılmasıyla sonuçlandırıldı. Donanım ve mekanik geliştirmenin ardından, yazılım geliştirme süreci de donanım entegrasyonu, iletişim yazılımı ve yer istasyonu yazılımı adımlarında üç ayrı fazda gerçekleştirildi.

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Cite This Article

Özgültekin, C., Turanlı, Y., Sadık, Ş. A. (2024). Design of a Model Satellite Consisting of Container and Payload for the Teknofest 2023 Competition. Journal of Scientific Reports-C, Sayı: 007, 10–24. https://ajindex.com/articles/1619149

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References (18)

  1. L. Kuzu, “Türkiye’de Uydu Teknolojilerinin Bugünü ve Geleceği,” Turkish Journal of Astronomy and Astrophysics, vol. 1, no. 2, p. 483-483, 2020.
  2. M. N. Sweeting, “Modern small satellites-changing the economics of space,” Proceedings of the IEEE, vol. 106, no. 3, pp. 343–361, 2018.
  3. L. Kuzu, A. F. Yagli, M. Gokten, and V. Yanikgonul, “Reliability analysis of TUSAT satellite communication payload,” in 2012 IEEE First AESS European Conference on Satellite Telecommunications (ESTEL), 2012, pp. 1–5. doi: 10.1109/ESTEL.2012.6400167.
  4. A. Baygeldi, “Ülkemizde Uydu ve Uzay Teknolojileri Alanında Faaliyetler ve Türkiye Uzay Ajansı Kurulum Çalışmaları,” in Turkish Journal of Astronomy and Astrophysics, Türk Astronomi Derneği, 2020, pp. 445–447.
  5. Ş. Kutlu, “Uydu-Uzay Teknolojilerinin Geliştirilmesinde Türkiye’nin Yönetim Anlayışı ve Dünya Ölçeğinde Karşılaştırmalı Bir Analiz,” Havacılık ve Uzay Çalışmaları Dergisi, vol. 1, no. 1, pp. 70–92, 2020.
  6. Ş. Gülgönül, E. Köklükaya, İ. Ertürk, and A. Y. Teşneli, “Aya: Haberleşme Uydusu Faydalı Yük Sistemi Akıllı Yedekleme Algoritması,” Gazi Üniversitesi Mühendislik Mimarlık Fakültesi Dergisi, vol. 29, no. 1, 2014.
  7. J. Praks et al., “Aalto-1, multi-payload CubeSat: Design, integration and launch,” Acta Astronaut, vol. 187, pp. 370–383, 2021, doi: https://doi.org/10.1016/j.actaastro.2020.11.042.
  8. D. J. Barnhart, T. Vladimirova, and M. N. Sweeting, “Very-small-satellite design for distributed space missions,” J Spacecr Rockets, vol. 44, no. 6, pp. 1294–1306, 2007.
  9. C. Çabuloğlu et al., “Mission analysis and planning of a CANSAT,” in Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011, 2011, pp. 794–799. doi: 10.1109/RAST.2011.5966951.
  10. S. N. Bulut et al., “Model satellite design for CanSat Competition,” in 2013 6th International Conference on Recent Advances in Space Technologies (RAST), IEEE, 2013, pp. 913–917.
  11. M. E. Aydemir, R. C. Dursun, and M. Pehlevan, “Ground station design procedures for CANSAT,” in 2013 6th International Conference on Recent Advances in Space Technologies (RAST), 2013, pp. 909–912. doi: 10.1109/RAST.2013.6581343.
  12. M. Ö. Kizilkaya, A. E. Oğuz, and S. Soyer, “CanSat descent control system design and implementation,” in 2017 8th International Conference on Recent Advances in Space Technologies (RAST), 2017, pp. 241–245. doi: 10.1109/RAST.2017.8002947.
  13. T. Islam, A. Noureen, M. R. Mughal, and M. A. Nadeem, “Design and Development of a Weather Monitoring Satellite, CanSat,” in 2019 15th International Conference on Emerging Technologies (ICET), 2019, pp. 1–6. doi: 10.1109/ICET48972.2019.8994718.
  14. R. P. Ramadhan, A. R. Ramadhan, S. A. Putri, M. I. C. Latukolan, Edwar, and Kusmadi, “Prototype of CanSat with Auto-gyro Payload for Small Satellite Education,” in 2019 IEEE 13th International Conference on Telecommunication Systems, Services, and Applications (TSSA), 2019, pp. 243–248. doi: 10.1109/TSSA48701.2019.8985514.
  15. A. Aborehab, M. Kassem, A. Nemnem, M. Kamel, and H. Kamel, “Configuration design and modeling of an efficient small satellite structure,” Engineering Solid Mechanics, vol. 8, no. 1, pp. 7–20, 2020.
  16. P. Shukla, R. Mishra, U. A. Sardar, and B. Mohapatra, “Satellite Design for CANSAT with Autorotatig payloads,” in 2022 4th International Conference on Advances in Computing, Communication Control and Networking (ICAC3N), 2022, pp. 2385–2392. doi: 10.1109/ICAC3N56670.2022.10074552.
  17. A. Aborehab, M. Kassem, A. F. Nemnem, and M. Kamel, “Structural optimization of a small earth remote sensing satellite,” Noise & Vibration Worldwide, vol. 54, no. 10–11, pp. 539–556, 2023.
  18. B. W. McCormick, Aerodynamics, aeronautics, and flight mechanics. John Wiley & Sons, 1994.