5 research outputs found

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

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    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

    Microcontroller Implementation for Automatic Smart Bell

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    This study aims to design automatic school bell hardware based on the ATmega32 microcontroller, design automatic school bell software based on the ATmega32 microcontroller using Basic programming language, and test the performance of the automatic school bell based on the ATmega32 microcontroller. This automatic school bell uses a minimum system of ATmega32 microcontrollers which equipped with data input from the push button, LCD to display character output, ISD2560 to output sound, and a timer taken from DS1307 RTC. This research is a Research or Development (R & D) research. This research is carried out through two stages of design. The first stage is the stage of hardware design. The second stage is the stage of software design. Programs are made using the Basic programming language using the Bascom-AVR application. The results of the product were tested using the black box method with two stages. In the first stage, software testing uses a series of simulations on the Proteus 7 Professional application. The second stage, testing hardware

    Wireless Monitoring Ketinggian Gelombang Laut Berbasis Sensor Inersial Measurement Unit

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    Pengembangan perangkat pengukur ketinggian gelombang laut secara wireless menggunakan sensor inersial measurement unit(IMU) menjadi fokus pembahasan dalam makalah ini. Prototipe dari perangkat yang dikembangkan serta pengujian fungsional dari rancangan perangkat disajikan dalam malakah ini. Pengembangan perangakat pengukur ketinggian gelombang laut secara wireless diakukan dengan membangun perangkat, menguji fungsional dari setiap bagian, menguji jarak jangkauan dari perangkat serta menganalisis pengiriman data sensor accelerometer dan gryrooscope. Pada makalah ini dibatasi pada efektifitas pembacaan dan pengiriman secara wireless data sensor percepatan dan Perubahan sudut dari pergerakan gelombang laut. Hasil pengujian menunjukkan perangkat pengukur ketinggian gelombang dari bentuk data mentah berupa accelerometer dan gyroscope dapat efektif dikirimkan sampai dengan jangkauan 3.8 km
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