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 …

This paper proposes a finite-time fault-tolerant trajectory tracking control for a quadrotor
system against external disturbances, parametric uncertainties and actuator faults without …

This paper proposes an adaptive barrier fast terminal sliding mode control (ABFTSMC)
approach for quadrotor unmanned aerial vehicles (UAV). Its main objectives are to mitigate …

This study proposes an adaptive barrier functions-based non-singular terminal sliding mode
control approach for the trajectory tracking of a quadrotor unmanned aerial vehicle subject to …

The past decades have witnessed an increase in the use of multirotor unmanned aerial
vehicles (UAVs). This has led the way to the development of fault-tolerant control algorithms …

In this article, an incremental guidancelaw with terminal angle constraint is proposed against
maneuvering targets in the 3-D space. First, a sliding surface is constructed such that its first …

In order to further expand the flight envelope of quadrotors under actuator failures, we
design a nonlinear sensor-based fault-tolerant controller to stabilize a quadrotor with failure …

In this work, a robust incremental three-dimensional (3D) guidance law is proposed
considering terminal angle constraint against maneuvering targets. As a stepping stone, the …

Presence of uncertainties caused by unforeseen malfunctions in actuation or measurement
systems or changes in aircraft behaviour could lead to aircraft loss-of-control during flight …

The emerging electric vertical take-off and landing aircraft (eVTOL) aircraft promotes the
convenient urban air mobility, but the maneuverability of the eVTOL has not gained …