Nonlinear model based particle swarm optimization of PID shimmy damping control

Alberto Milazzo, Calogero Orlando, Andrea Alaimo

Risultato della ricerca: Articlepeer review

5 Citazioni (Scopus)

Abstract

he present study aims to investigate the shimmy stability behavior of a single wheeled nose landing gear system. The system is supposed to be equipped with an electromechanical actuator capable to control the shimmy vibrations. A Proportional-Integrative-Derivative (PID) controller, tuned by using the Particle Swarm Optimization (PSO) procedure, is here proposed to actively damp the shimmy vibration. Time-history results for some test cases are reported and commented. Stochastic analysis is last presented to assess the robustness of the control system.
Lingua originaleEnglish
pagine (da-a)211-224
Numero di pagine14
RivistaAdvances in Aircraft and Spacecraft Science
Volume3
Stato di pubblicazionePublished - 2016

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Fluid Flow and Transfer Processes

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