Now showing items 1-2 of 2
Output Feedback Sliding Mode Control of a Fixed-Wing UAV Under Rudder Loss
(American Institute of Aeronautics and Astronautics Inc, AIAA, 2019-01)
The purpose of this study is to design a Dynamic discrete output feedback SMC for fixed wing aircraft under rudder loss operation. Recently, UAVs have been utilized in many commercial and military applications. However, ...
Comparative analysis of performance of the SEPIC converter using LQR and PID controllers
(Institute of Electrical and Electronics Engineers Inc., 2017-11)
The purpose of this study is to design a LQR controller for the SEPIC (Single-Ended Primary-Inductor Converter) converter which is widely employed in industrial DC-DC power conversion and is also starting to see widespread ...