Quadrotor Unmanned Aerial Vehicle (UAV) is an unstable system, so it needs to be
controlled efficiently and intelligently. Moreover, due to its non-linear, coupled, and under …

Based on the predigestion of the dynamic model of the intelligent firefighting vehicle, a linear
2‐DOF lateral dynamic model and a preview error model are established. To solve the …

In this paper, a new optimal reduced order fractionalized PID (ROFPID) controller based on
the Harris Hawks Optimization Algorithm (HHOA) is proposed for aircraft pitch angle control …

In this study, Harris hawks optimization (HHO) algorithm has been proposed as a novel meta-
heuristic algorithm to achieve optimal parameters of a PID controller adopted for aircraft …

This paper presents the design of an artificial neural network (ANN) and proportional
integral derivative (PID) controller using particle swarm optimization (PSO) for Boeing 747 …

Controlling the pitch angle of an aircraft holds paramount importance in the aviation industry,
where pilots are tasked with maintaining specific attitudes for straight and level flight, as well …

Stability of power converters has always been a major concern when dealing with nonlinear
behavior of the system and swarm-based optimization techniques are proven to be handy as …

This paper investigates the overload stabilization problem of the rolling-missile subject to
parameters uncertainty and actuator saturation. In order to solve this problem, a sliding …

To overcome the effect of floating platform heave motion on the drilling operation, a new
crown-block heave compensation system with compound cylinders is developed. The new …

This research represents the Proportional integral derivative (PID) as well as linear
quadratic regulator (LQR) controllers that are devised in the favor of an aircraft's pitch control …