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| Title | : | Flight Trajectory Control System on Fixed Wing UAV using Linear Quadratic Regulator |
| Author | : |
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) |
| Date | : | 0 2019 |
| Keyword | : | LQR,UAV,Control LQR,UAV,Control |
| 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. |
| Group of Knowledge | : | Teknik Kendali (Atau Instrumentasi dan Kontrol) |
| Original Language | : | English |
| Level | : | Internasional |
| Status | : |
Published
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Flight Trajectory Control System on Fixed Wing UAV using Linear Quadratic Regulator.pdf
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