Paper Title:
Semi-Active Landing Gear with MR Fluid Damper Based on ADAMS&MATLAB Co-Simulation
  Abstract

According to MR fluid properties and MR damper structure, a multi-body dynamic model of semi-active landing gear was built by using virtual prototype in ADMAS/Aircraft. Fuzzy control system for the semi-active landing gear with MR damper was designed under the MATLAB/Simulink environment. Co-Simulation of ADAMS/Aircraft and MATLAB/Simulink were carried out. The simulation results show that semi-active landing gear with MR damper based on fuzzy control strategy can reduce the aircraft’s vibration and improve the ride comfort characteristics. Co-simulation method provides one simple feasible method for the process of landing gear design, development and manufacture. It also offers a new way to advance designing quality for complex dynamic system and control strategy simulation.

  Info
Periodical
Advanced Materials Research (Volumes 228-229)
Edited by
Quanjie Gao
Pages
363-367
DOI
10.4028/www.scientific.net/AMR.228-229.363
Citation
S. S. Pawale, H. J. Wang, "Semi-Active Landing Gear with MR Fluid Damper Based on ADAMS&MATLAB Co-Simulation", Advanced Materials Research, Vols. 228-229, pp. 363-367, 2011
Online since
April 2011
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Price
$32.00
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