Micro-Unmanned Air Vehicles (Micro-UAVs), especially quadrotor UAVs, have been widely
used in recent years because of their simple structure and convenient operation. However …

This study investigates the relative impacts of different gusts on representative small
Uncrewed Air Systems through the use of a simple analytical model. The model uses basic …

This paper addresses flight stability and performance in wind of a quadrotor equipped with
custom flow probes that measure the wind velocity. Wind-velocity measurements are used in …

This paper describes a novel multirotor unmanned aerial vehicle aerodynamic force model
with the aim of creating a multirotor simulation that is suitable for the evaluation of station …

In this paper, an anti-disturbance output tracking control strategy is proposed for turbofan
systems with multiple disturbances. The considered turbofan models are described by …

A new output tracking (OT) control strategy is established for the turbofan systems involved
by multiple disturbances, the measurable disturbance and unmeasurable disturbance. The …

The small unmanned aerial vehicles are susceptible to wind disturbances due to the
turbulent environment at their low operational altitude. Compared to conventional IMU …

This paper presents a bioinspired approach for fast reaction to external disturbances as
applied to small unmanned aerial systems platforms. A disturbance rejection method for a …

1 β0= blade coning angle, rad β1c= longitudinal blade flapping angle, rad β1s= lateral blade
flapping angle, rad βmax= maximum blade flap angle, rad γ= Lock number θ0= blade root …

In the past three decades, numerous works have been done on the applications of linear
and nonlinear Kalman filters in estimating crewed and uncrewed aircraft airflow angles. In …