Flight Attitude Characteristic Analysis Of LSU-01 Without Control System

Eko Budi Purwanto (2013) Flight Attitude Characteristic Analysis Of LSU-01 Without Control System. Proceedings SIPTEKGAN XVII-2013. pp. 45-54. ISSN 978-979-1458-74-0

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The paper present the modeling of dynamic characteristic of UAV. The dynamic model was developed using first principle method. The flight dynamic parameter is calculated using Datcom and the dynamic characteristic is analyzed usingMatlab software. The simulation shows that the real part of eigenvalue LSU-01 is on the left of imaginary axis, which means that the system has static and dynamic stability. The place pole of LSU-01 in the s-plane shows similarity with common aircraft mode.

Item Type: Article
Uncontrolled Keywords: modeling, flight dynamic, datcom, LSU-01
Subjects: Teknologi Penerbangan dan Antariksa > Penelitian, Pengembangan, Perekayasaan, dan Pemanfaatan > Teknologi Aeronautika
Divisions: Deputi Teknologi Penerbangan Dan Antariksa > Pusat Teknologi Penerbangan
Depositing User: Een Rohaeni
Date Deposited: 24 Mar 2021 04:00
Last Modified: 24 Mar 2021 04:00
URI: http://repositori.lapan.go.id/id/eprint/493

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