High Altitude Balloon Payload Design for Atmospheric Observations

Authors

  • Rama Okta Wiyagi Department of Electrical Engineering, Universitas Muhammadiyah Yogyakarta
  • . Danardono Department of Electrical Engineering, Universitas Muhammadiyah Yogyakarta
  • Try Ahmad Agus Department of Electrical Engineering, Universitas Muhammadiyah Yogyakarta

DOI:

https://doi.org/10.18196/jet.1107

Keywords:

high altitude balloon payload, atmospheric parameter, air pressure, temperature, relative humidity, telemetry

Abstract

In 2016, Microcontroller Research Group at Dept. of Electrical Engineering Universitas Muhammadiyah Yogykarta has designed and developed a payload for High Altitude Balloon. This payload has function measuring atmospheric parameter vertically and sending the data to ground station on earth using telemetry. The parameters measured are air pressure, temperature and relative humidity. Besides sending these parameters, payload also have mission monitoring real positions of payload using GPS, real time video transmission,regulary capturing and sending image from payload . This payload is tested on the annual Atmosphere Balloon Payload Competition (KOMBAT) 2016. This paper will describe the design payload, payload software algorithms and the results that have been obtained. 

References

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How to Cite

Wiyagi, R. O., Danardono, ., & Agus, T. A. (2018). High Altitude Balloon Payload Design for Atmospheric Observations. Journal of Electrical Technology UMY, 1(1), 50–57. https://doi.org/10.18196/jet.1107

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Articles