Akuisisi Data dan Kalibrasi pada Sistem Can Satellite (Cansat)

Authors

  • Muhammad Jaka Wimbang Wicaksono Politeknik Negeri Batam
  • Eka Mutia Lubis Politeknik Negeri Batam
  • Dessy Oktani Politeknik Negeri Batam
  • Kamarudin Kamarudin Politeknik Negeri Batam
  • Aditya Gautama Darmoyono Politeknik Negeri Batam
  • Rahmi Mahdaliza Politeknik Negeri Batam
  • Mu’thiana Gusnam Politeknik Negeri Batam
  • Ahmad Syafi’i Politeknik Negeri Batam
  • Muhammad Naufal Airlangga Diputra Politeknik Negeri Batam
  • Danu Satia Nugraha Politeknik Negeri Batam
  • Muhamad Shafiq Abrajano Politeknik Negeri Batam
  • Rezza Eka Syahputra Politeknik Negeri Batam

DOI:

https://doi.org/10.30871/ji.v17i1.9348

Keywords:

Cansat, Data acquisition, Callibration, Flight Software

Abstract

This study aims to develop and test a data acquisition and calibration system for CanSat, a small nanosatellite designed as a cost-effective solution for collecting geographical and spatial data. CanSat collects data using BME-280, MPU-9250, and NEO-6M sensors, then transmits it via XBee to a GUI for controlling the release of the Heat Shield, parachute, and legs. The data is analyzed using statistical methods and transmitted via XBee S2C. The results show that the BME-280 has a standard error of 0.35 and a deviation of 0.77 for temperature, and a standard error of 0.06 with a deviation of 0.13 for air pressure. The altitude measurement has a standard error of 0.02 and a deviation of 0.05. Meanwhile, MPU-9250 has an average standard error of 0.34 and a deviation of 0.77 for angle orientation measurement. The design and testing of the leg control system conclude that it functions at 80% efficiency.

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References

[1] B. P. Wibowo, D. Gunawan, T. Siahaan, and U. Pertahanan, “Pengembangan Satelit A3 Untuk Mendukung Sistem Pertahanan Negara,” J. Ind. Pertahanan, vol. 2, pp. 200–221, 2020.

[2] J. Lambert, R. Monahan, and K. Casey, “Power Consumption Profiling Of a Lightweight Development Board: Sensing With The INA219 and Teensy 4.0 Microcontroller,” Electron., vol. 10, no. 7, 2021.

[3] M. Bakirci and M. M. Özer, “An IoT-Based Modular Avionics and Electrical System for Nanosatellite Systems,” ICCIDA 2022 Comput. Intell. Data Anal. Appl., vol. 643, pp. 218–229, 2023.

[4] T. Suryana, “Antarmuka UBlox NEO-6M GPS Module dengan NodeMCU ESP8266,” J. Komputa Unikom, pp. 1–18, 2021. Available: https://repository.unikom.ac.id/

[5] P. Kaewnoen, “Simulation of Life Supporting Conditions on Exoplanets by CanSat,” pp. 1–4, 2021.

[6] M. Bakırcı and M. Özer, "An iot-based modular avionics and electrical system for nanosatellite systems", Lecture Notes in Networks and Systems, p. 218-229, 2023. https://doi.org/10.1007/978-3-031-27099-4_17

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Published

2025-04-30

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