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ITS » Undergraduate Theses » Teknik Mesin
Posted by ansi@its.ac.id at 23/01/2013 13:14:42  •  1086 Views


KOMPARASI SISTEM KONTROL SATELIT ADCS DENGAN METODE KONTROL PID DAN SLIDING-PID

PID AND SLIDING-PID METHODS COMPARATION OF SATELLITE CONTROL SYSTEM ADCS

Author :
NUR, IMROATUL UST ( 2108100165 )




ABSTRAK

Wilayah Indonesia yang begitu luas membutuhkan suatu alat yang dapat digunakan untuk memantau keamanan laut dan pertahanan pengamatan obyek dan komunikasi yaitu satelit. Satelit tersusun atas beberapa sub-sistem yang sangat kompleks. ADCS Attitude Determination and Control System merupakan salah satu sub-sistem yang memerlukan kontrol otomatis. Oleh karena itu dibutuhkan suatu sistem kendali yang paling sesuai dalam menjaga kestabilan ADCS guna mengatur orientasi satelit pada saat bergerak mengelilingi bumi. Pada penelitian ini dilakukan perancangan sistem kendali Sliding-PID untuk menstabilkan ADCS. Sliding-PID merupakan gabungan dari kendali PID dan Sliding Mode Controller. Pemodelan sistem ADCS dilakukan dengan menggunakan Simulink Matlab berdasarkan persamaan kinematika dan dinamika. Hasil dari implementasi kendali Sliding-PID pada simulasi menunjukkan bahwa dalam menstabilkan ADCS Sliding-PID mampu mencapai kestabilan 6822 lebih cepat daripada kendali PID biasa serta mampu mengurangi error yang terjadi hingga 7846 9643 dan 40 untuk sudut x sudut y dan sudut z.


ABSTRACT

Indonesia has a very vast territory. Therefore a device is needed to monitor the offshore safety and defense system object surveillance and communication. A device that can do all those important things is a satellite. A satellite consists of several complex subsystems. ADCS Attitude Determination and Control System is one of these subsystem in which an automatic control is needed. Hence a reliable control system is required to keep the ADCS steady as it adjusts the satellite orientation. The design of sliding-PID control system for stabilizing the ADCS is carried out in this study. Sliding-PID is a combination of PID controller and sliding mode controller. The ADCS modelling is done using Simulink Matlab according to kinematics and dynamics equations. The result of Sliding-PID controller implementation simulation shows that the Sliding-PID is 6822 faster than the classic PID in stabilizing the ADCS and is able to reduce te error up to 7846 9643 and 40 for angle of x y and z respectively .



KeywordsSatelit; ADCS; Kendali PID; Sliding-PID
 
Subject:  PID controllers Artificial satellites--attitude control systems
Contributor
  1. HENDRO NURHADI, Dipl.-Ing., Ph.D.
Date Create: 24/07/2012
Type: Text
Format: pdf
Language: Indonesian
Identifier: ITS-Undergraduate-21001130001877
Collection ID: 21001130001877
Call Number: RSM 629.89 Nur k


Source
Undergraduate Thesis of Mechanical Engineering, RSM 629.89 Nur k, 2013

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Copyright @2013 by ITS Library. This publication is protected by copyright and per obtained from the ITS Library prior to any prohibited reproduction, storage in a re transmission in any form or by any means, electronic, mechanical, photocopying, reco For information regarding permission(s), write to ITS Library




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  1.  ITS-Undergraduate-23553-abstract-idpdf.pdf - 242 KB
  2.  ITS-Undergraduate-23553-Abstract_en-pdf.pdf - 242 KB
  3.  ITS-Undergraduate-23553-conclusionpdf.pdf - 193 KB




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