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All Journal Jurnal Pertahanan : Media Informasi tentang Kajian dan Strategi Pertahanan yang Mengedepankan Identity, Nasionalism dan Integrity Jurnal Pendidikan Teknologi Pertanian Aviation Electronics, Information Technology, Telecommunications, Electricals, and Controls (AVITEC) Jurnal Dedikasi Bhakti Nagori (Jurnal Pengabdian kepada Masyarakat) Vokatek : Jurnal Pengabdian Masyarakat Jurnal Pengabdian Masyarakat Micronic: Journal of Multidisciplinary Electrical and Electronics Engineering
Mudarris Mudarris
Universitas Negeri Makassar
Aerospace Engineering Agriculture, Biological Sciences & Forestry Humanities Chemical Engineering, Chemistry & Bioengineering Civil Engineering, Building, Construction & Architecture Computer Science & IT Control & Systems Engineering Economics, Econometrics & Finance Education Electrical & Electronics Engineering Engineering Environmental Science Languange, Linguistic, Communication & Media Mechanical Engineering Social Sciences Other

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Implementasi Sensor Inertial Measurement Unit (IMU) untuk Monitoring Perilaku Roket Mudarris Mudarris; Satria Gunawan Zain
Aviation Electronics, Information Technology, Telecommunications, Electricals, Controls (AVITEC) Vol 2, No 1 (2020): February
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.28989/avitec.v2i1.610

Abstract

This paper examines the Implementation of the Inertial Measurement Unit (IMU) Sensor for Monitoring Rocket Attitude. The monitored rocket attitude data is in the form of vibration which is generated by the payload during the functional test and flight speed, acceleration and direction flight test. The rocket payload device is mounted in the rocket compartment for the function of measuring rocket behavior. Data is sent to ground stations via telemetry devices use baud rate of 57600. Based on the results of G-Shock, G-Force and Vibration testing shows that the payload can work well. In accordance with the results of reading the data on the Graphical user Interface (GUI) can be displayed and shows the rocket payload works well. This rocket payload can transmit data remotely. 
Co-Authors Akmal Hidayat Akmal Hidayat Aminuddin Aminuddin Askar, Ambo Ayusnin, Siti Reski Dewi Triantini Faisal, Andi Nur Fathahillah Fathahillah Fiskia Rera Baharuddin Hamidah Hamris Hartini Ramli Ika Wisudawaty Iris Sumariyanto Misbahuddin, Azizah Fauziah Muhammad Haristo Rahman Muhammad Hasim Muhammad Hasim S Muhammad Romario Basirung Munzir Munzir Nuran, Andi Shridivia Sri Wahyuni Sumariyanto, Iris Sumariyanto, Iris Udin Ummul Mansir WAHYUDI Wahyudi Wahyudi Wulan Purnamasari