Study on Variable Universe Fuzzy PID Control for Landing Gear Based on MRF (Magneto-Rheological Fluid) Damper

Shi Xing Zhu; Chan Juan Chen

doi:10.4028/www.scientific.net/AMM.233.66

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Structural Design and Simulation Optimization of New Type Telescoping Heavy Hydraulic Trailer Steering System
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Dual-Pump Hydraulic Hybrid Excavator with Combined Common Pressure Rail and Valve-Controlled System
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Study on Variable Universe Fuzzy PID Control for Landing Gear Based on MRF (Magneto-Rheological Fluid) Damper
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 233Study on Variable Universe Fuzzy PID Control for...

Study on Variable Universe Fuzzy PID Control for Landing Gear Based on MRF (Magneto-Rheological Fluid) Damper

Abstract:

Aircraft landing gear shock system model was established, The system vibration differential equation and state-space equation were deserved。Based on the general fuzzy PID controller, the idea of fuzzy PID controller and its application in shock absorber system were studied. Based on MATLAB, the system simulation model was established, and the fuzzy PID control of semi-active suspension is analyzed compared to variable universe fuzzy PID control. The results show that the variable universe fuzzy PID control had better control effect.

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Periodical:

Applied Mechanics and Materials (Volume 233)

Pages:

66-71

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.233.66

Citation:

Cite this paper

Online since:

November 2012

Authors:

Shi Xing Zhu, Chan Juan Chen

Keywords:

Fuzzy PID-Control, Landing Gear, Simulation, Variable Universe

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