Now showing items 1-5 of 5
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, ...
Design of a 4D Trajectory Tracking Controller with Anti-Windup Protection for Fixed-Wing Aircraft
(Institute of Electrical and Electronics Engineers Inc., 2019-10)
This work contains the design and test of a control scheme for a fixed-wing aircraft to track 4-dimensional waypoints. The controller scheme is a multi-loop design that consists of an inner controller synthesized with the ...
Heading hold autopilot design for fixed wing aircraft
(American Institute of Aeronautics and Astronautics Inc, AIAA, 2018-01)
Interest for autopilot design has become a rich subject in light of recent developments. There may be mixed use of the so-called modern and classical control strategies as to the design of an autopilot for any specific ...
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 ...
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. ...