Indonesian Journal of Aerospace
Vol. 10 No. 2 Desember (2012): Jurnal Teknologi Dirgantara

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

Purwanto, Eko Budi (Unknown)
Nasution, Syahron Hasbi (Unknown)
Supendi (Unknown)

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.

Copyrights © 2012




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Journal Info
Indonesian Journal of Aerospace
Website

Abbrev

ijoa

Publisher

Badan Riset dan Inovasi Nasional

Subject

Aerospace Engineering Astronomy

Description

Indonesian Journal of Aerospace provides a broad opportunity for the scientific and engineering community to report research results, disseminate knowledge, and exchange ideas in various fields related to aerospace science, technology, and policy. Topics suitable for publication in the IJoA include ...