Jurnal Teknologi Dirgantara
Vol.10 No.2 Desember 2012

IDENTIFIKASI PARAMETER DAN PERANCANGAN SISTEM KENDALI PID UNTUK ANALISIS SIKAP TERBANG UAV [PARAMETER IDENTIFICATION AND DESIGN PID CONTROLLER FOR FLYING ATTITUDE ANALYSIS OF UAV]

Eko Budi Purwanto (Bidang Simulasi dan Pemodelan, Pustekbang, Lapan)
Syahron Hasbi Nasution (STEI – ITB)
- Supendi (STEI – ITB)

Article Info

Publish Date
15 Mar 2013

Abstract

Based on the state space yield first principle method knowed that characteristic of UAV is static stable. To get the near real condition doing verification of state space model by using the identification system toolbox of Matlab. The yield show that matrix element of state space is different both of them. Furher step is design the PID control system base on new state space, and for improve the performance system used Kalman filter. Key word: identification system, PID parameter, Kalman filter, Maximum overshoot

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Journal Info
Jurnal Teknologi Dirgantara
Website

Abbrev

jurnal_tekgan

Publisher

Lembaga Penerbangan dan Antariksa Nasional

Subject

Aerospace Engineering Chemical Engineering, Chemistry & Bioengineering Computer Science & IT Mechanical Engineering Physics

Description

Jurnal Teknologi Dirgantara (Journal of Aerospace Technology) is an Indonesian accredited scientific publication that covers topics of Rocket, satellite, and aeronautics technology, as well as a spin-off from aerospace technology, such as aerodynamics, astronautics, aerospace structure, power and ...