Implementasi Sensor Inertial Measurement Unit (IMU) untuk Monitoring Perilaku Roket


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Title Implementasi Sensor Inertial Measurement Unit (IMU) untuk Monitoring Perilaku Roket
Creator Mudarris, Mudarris
Zain, Satria Gunawan
Subject Teknik Elektro
Payload, Rocket Attitude, IMU, Monitoring, Rocket
Description 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. 
Publisher Sekolah Tinggi Teknologi Adisutjipto
Contributor Universitas Negeri Makassar Department Pendidikan Teknik Elektro
Date 2020-02-03
Type info:eu-repo/semantics/article
Peer-reviewed Article
Format application/pdf
Source AVITEC; Vol 2, No 1 (2020): Februari 2020; 55-64
Language eng
Rights Copyright (c) 2020 AVITEC

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