Flight Trajectory Control System on Fixed Wing UAV using Linear Quadratic Regulator
Penulis/Author
Prof. Dr. Techn. Ahmad Ashari, M.I.Kom. (1); HAFIZNA ARSYIL FADHLI (2); Dr. Andi Dharmawan, S.Si., M.Cs. (3); Ariesta Martiningtyas Handayani, S.Si., M.Cs. (4)
Tanggal/Date
2019
Kata Kunci/Keyword
Abstrak/Abstract
Utilization of Unmanned Aerial Vehicle (UAV)
technology has developed rapidly over the past decade. Its use is
no longer limited to the military field but has covered various
aspects of human work. One type of UAV that is widely used is a
type of fixed wing. This type of UAV has the advantage of being
able to maneuver with 6 Degree of Freedom (DoF) by utilizing
deflections from its surface controls. The surface controls of this
UAV consist of an elevator, a rudder, and two ailerons. By
utilizing all of the surface controls, the UAV is expected to fly
according to the specified flight path. Therefore, flight control
systems are needed. Linear Quadratic Regulator (LQR) is an
optimal control that can be used to maintain lateral and
longitudinal attitude stability of the UAV while tracing the
waypoint coordinates. The results of the study show the response
of the system under the desired specifications. These results
indicate that the control system has been able to maintain vehicle
stability while tracing the path along with the waypoints.
Rumpun Ilmu
Teknik Kendali (Atau Instrumentasi dan Kontrol)
Bahasa Asli/Original Language
English
Level
Internasional
Status
Dokumen Karya
No
Judul
Tipe Dokumen
Aksi
1
Flight Trajectory Control System on Fixed Wing UAV using Linear Quadratic Regulator.pdf
