PERANCANGAN ROKET KENDALI DAN SISTEM TRANSFER DATA DENGAN USER INTERFACE MENGGUNAKAN AMP PLANNER ( ROCKET DESIGN CONTROL AND DATA TRANSFER SYSTEM WITH USER INTERFACE USING AMP PLANNER )

Hartadi S, Raisqi Kun and Wahyunaeni, Hafidz Ari and Mugiharjo , Tri Rinanto and Aprilianto, Sigit and Setyoko, Bambang (2014) PERANCANGAN ROKET KENDALI DAN SISTEM TRANSFER DATA DENGAN USER INTERFACE MENGGUNAKAN AMP PLANNER ( ROCKET DESIGN CONTROL AND DATA TRANSFER SYSTEM WITH USER INTERFACE USING AMP PLANNER ). Undergraduate thesis, D3 Teknik Mesin.

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Abstract

Pada tugas akhir ini dilakukan perancangan dan pembuatan roket EDF yang bertujuan untuk pengambilan sebuah data (roll, pitch, dan yaw) dengan sistem pendeteksi rotasi menggunakan gyroscope berbasis mikrokontroler MultiWii PRO 3329 untuk mendeteksi sudut rotasi dari ketiga poros putar. Data berupa sudut diperoleh dari hasil integral terhadap keluaran gyroscope yang berupa sinyal kecepatan sudut. Sensor gyroscope memiliki kelebihan yaitu sensor ini tidak bersentuhan langsung secara fisik dengan lingkungan sekitar sehingga sangat cocok digunakan pada benda yang bergerak bebas. Dari hasil penyelesaian tugas akhir yaitu perancangan roket kendali dan sistem data dengan user interface menggunakan AMP Planner, maka dapat kami simpulkan beberapa hal antara lain: perlu adanya sistem transfer data untuk mengendalikan sikap roket dan mekanisme peluncuran roket kendali pada saat roket diluncurkan. Adapun hasil data yang di dapat sebagai berikut : sikap roket pitch -80.99° roll -44.22° yaw 189.98°, Daya dorong motor listrik 310W @ 11.1V (3S) / 696W @ 15V (4S0, putaran motor listrik 2200 rpm/v . Kata kunci : Roket EDF, Sistem Telemetri, Roll Pitch Yaw. In this final project to design and manufacture EDF rocket aimed to capture the data (roll, pitch, and yaw) with a detection system using gyroscope-based rotation MultiWii PRO 3329 microcontroller to detect the angle of rotation of the third rotary shaft. The data obtained from the corner in the form of an integral of the gyroscope output signal in the form of angular velocity. Gyroscope sensor has the advantages of this sensor is not in direct contact with the physical environment so it is suitable for use in freely moving object. From the result of the completion of the final project is the design of rocket control and data system with a user interface using AMP Planner, then we can conclude several things, among others: the need for a system of data transfer for attitude control rocket and mechanisms rocket launch control at the time of the rocket launch, The results the data can be as follows: -80.99 ° pitch attitude rocket roll 189.98 ° -44.22 ° yaw, thrust electric motor 310W @ 11.1V (3S) / 696W @ 15V (4S0, electric motor rotation 2200 rpm / v. Key Words : EDF Rocket, Telemetry System, Roll Pitch Yaw.

Item Type:Thesis (Undergraduate)
Subjects:T Technology > TJ Mechanical engineering and machinery
Divisions:Faculty of Engineering > Diploma in Mechanical Engineering
Faculty of Engineering > Diploma in Mechanical Engineering
ID Code:44919
Deposited By:Mrs Wahyu D3 Teknik Mesin
Deposited On:29 Dec 2014 08:58
Last Modified:29 Dec 2014 08:58

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