Arga C. Pamungkas, Alma A. Putra, Pradini Puspitaningayu, Yulia Fransisca, Arif Widodo
A rocket system generally consists of two parts, the rocket motor and the payload. The payload system is built of several sensors such as accelerometer, gyroscope, magnetometer, and also a surveillance camera. These sensors are used to monitor the rocket in a three-dimensional axis which determine its attitude. Additionally, the payload must be able to perform image capturing in a certain distance using telecommand. This article is intended to describe the design and also the implementation of a rocket payload which has attitude monitoring and telecommand ability from the ground control station using a long-range wireless module Digi XBee Pro 900 HP. © 2018 Institute of Physics Publishing. All rights reserved.
Department of Electrical Engineering, Faculty of Engineering, Universitas Negeri Surabaya, Indonesia
