Milad Zarchi

TL;DR: In this article, a proportional integral derivative technique for control of an active vibration absorber system using a hydraulic nonlinear actuator based on the bees algorithm is proposed, which is inspired by the natural intelligent foraging behaviour of honey bees.

TL;DR: Results of system numerical Simulation with optimized controller using Bees Algorithm in MATLAB software shows that the transmitted impact load to airframe, the vertical vibration of aircraft and time to return static equilibrium position at touchdown are significantly improved compared with other control performances.

TL;DR: In this paper, a controller for a second order system based on Linear Quadratic Regulator (LQR) was designed for active landing gear system that chooses damping and stiffness performance of suspension system as control object.

TL;DR: The results of numerical analysis for this large-scale airplane model with six degrees of freedom demonstrate that the active shock absorber system in accordance with two types of the bee multi-objective algorithm has good performance in comparison with the passive approach to minimize the bounce displacement and momentum.

TL;DR: Design of Proportional Integral Derivative controller based on Bees Intelligent Algorithm as the optimization technique for nonlinear model of semi-active landing gear system that chooses damping performance of system at touchdown as object function and results are significantly improved.