In this study, for the purpose of finite-time tracking control of quad-rotor Unmanned Aerial
Vehicle (UAV) system under modeling uncertainties and external disturbances, an adaptive …

Adaptive control methods are developed for stability and tracking control of flight systems in
the presence of parametric uncertainties. This paper offers a design technique of adaptive …

In this paper, a 6-Degrees-of-Freedom (6-DOF) Unmanned Aerial Vehicle (UAV) system with
external disturbance corresponding to sensor failure is considered. The control method is …

This paper proposes an active fault-tolerant control strategy for a quadrotor helicopter
against actuator faults and model uncertainties while explicitly considering fault estimation …

Unmanned air vehicles are intrinsically non-linear, unstable, uncertain, and prone to a
variety of faults, most commonly the motor faults. The main objective of this paper is to …

In this research, a novel adaptive non-singular terminal sliding mode control (ANTSMC) is
proposed for finite-time attitude and altitude tracking of aircraft system considering the …

In this article, a sliding mode control based on neural networks is proposed for attitude and
altitude system of quadcopter under external disturbances. First, the dynamic model of the …

This paper presents a reliable and novel quadrotor flight control system designed to
enhance trajectory tracking performance, robustness and adaptiveness against the …

We present a robust adaptive second-order sliding mode controller that rejects external
disturbances and uncertainties to improve the tracking performance of attitude and altitude …

In this article, an adaptive neural fault-tolerant control (FTC) scheme is proposed for the
medium-scale unmanned autonomous helicopter subject to external disturbance, actuator …