In recent times, technological advancement boosts the desire of utilizing the autonomous
Unmanned Aerial Vehicle (UAV) in both civil and military sectors. Among various UAVs, the …

A quadcopter is underactuated where there are 6° of motion with only four rotors to control
all six motions. Varying the speed of the four rotors can produce thrust, roll, pitch and yaw …

This paper presents a proportional-integral-derivative (PID) flight controller for a quadrotor
micro air vehicle (MAV). The MAV (Parrot Mambo minidrones) is small, therefore, a slight …

In this paper, a fuzzy model predictive controller based on disturbance observer is proposed
for attitude control of quadrotor Unmanned Aerial Vehicle (UAV) subject to input constraints …

The development of Unmanned Aerial Vehicles (UAVs) has become one of the most fruitful
research areas in the field of autonomous flight control. Quadcopters are chosen due to their …

This paper provides a comparative study of three Sliding Mode Control (SMC)-based fault
tolerant controllers for trajectory tracking of a quadrotor UAV subject to actuator faults …

Unmanned aerial vehicles (UAVs) have garnered more attention across various industries in
recent years, leading to significant development in their design and application globally …

A fault tolerant control approach is proposed in this paper for quadrotor Unmanned Aerial
Vehicle (UAV) subject to time varying disturbances and actuator faults. The approach is …

The main difficulty in the traditional nonlinear H∞ control design lies in how to solve the
nonlinear partial differential Hamilton-Jacobi-Isaacs equation (HJIE), especially for …

This paper proposes the design of a PID controller for the position and attitude stabilization
of a quadrotor unmanned aerial vehicle (UAV) using the differential-evolution (DE) …