Waypoint Tracking of a FixedWing UAV Using the L1 Cross Track Error Control
Penulis/Author
Prof. Gesang Nugroho, ST., MT., Ph.D. (1); Dr. Andi Dharmawan, S.Si., M.Cs. (2); Dr. Danang Lelono, S.Si., M.T. (3); Ariesta Martiningtyas Handayani, S.Si., M.Cs. (4)
Tanggal/Date
2022
Kata Kunci/Keyword
Abstrak/Abstract
The utilization of fixed-wing Unmanned Aerial Vehicle (UAV) technology has
grown not limited to the military field but also in monitoring, mapping and aerial
photography. One of the activities that are often carried out is monitoring the area and
aerial photography. To carry out this mission, the UAV must be able to trace the waypoint
lines. The waypoint control system made in this study uses the Linear Quadratic Regulator
(LQR) method to maintain the stability of the lateral and longitudinal attitudes of the vehicle
during the waypoint tracking mission. In navigation control, the L1 controller method
generates the value of lateral acceleration and is converted into an angle value to navigate
the UAV to the waypoint line. The results of this study are the UAV can maintain the
trajectory while simultaneously tracking the six waypoint coordinates autonomously using
the Linear Quadratic Regulator (LQR) and the L1 controller navigation method.
Rumpun Ilmu
Sistem Informasi Geografi (SIG)
Bahasa Asli/Original Language
English
Level
Internasional
Status
Dokumen Karya
No
Judul
Tipe Dokumen
Aksi
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ICIC-WAYPOINT TRACKING OF A FIXED-WING UAV USING THE L1 CROSS TRACK ERROR CONTROL.pdf
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WAYPOINT TRACKING OF A FIXED-WING UAV USING THE L1 CROSS TRACK ERROR CONTROL.pdf