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

S. S. Pawale; Hai Jun Wang

doi:10.4028/www.scientific.net/AMR.228-229.363

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 228-229Semi-Active Landing Gear with MR Fluid Damper...

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.

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Periodical:

Advanced Materials Research (Volumes 228-229)

Pages:

363-367

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.228-229.363

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Online since:

April 2011

Authors:

S. S. Pawale, Hai Jun Wang

Keywords:

Fuzzy Control, Magnetorheological Fluid (MRF), MR Damper, Semi-Active Landing Gear

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