Now showing items 1-3 of 3
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, ...
Stabilizer Autopilot Design For Fixed Wing UAV Using ODSMC
In this paper we build an ODSMC (Output Feedback Discrete Time Sliding Mode Control) controller for a fixed-winged aircraft. ODSMC control is employed, which is widely utilized in commercial and reconnaissance applications. ...
Rudder Loss Recovery Autopilot System for a Small Fixed-Wing Aircraft
This paper presents an integrated way of development of an aircraft dynamic modeling including stability and control derivatives and ensuing autopilot design. Stability derivatives are calculated via an automated procedure ...