Slid Mode VSC for Aircraft Anti-Skid Braking System with Index Reaching Law

Long Fei Fu; Yu Ren Li; Guang Lai Tian; Bo Liang; Hong Ling Wang

doi:10.4028/www.scientific.net/AMM.336-338.973

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 336-338Slid Mode VSC for Aircraft Anti-Skid Braking...

Slid Mode VSC for Aircraft Anti-Skid Braking System with Index Reaching Law

Abstract:

Aircraft anti-skid braking system providing protection for the safety of the aircraft landed by controlling the brake pressure to be maintained slip ratio in best condition. The aircraft anti-skid braking system is hard to control as the nonlinear model of the aircraft dynamics, the uncertainty of friction between the tires and the ground of braking process. With the study of slip ratio and research of aircraft anti-skid braking system dynamics model, the sliding mode variable structure controller is designed. Then index reaching law is adopted to eliminate the system chattering and the performance is analyzed, further more the robustness is strengthen. Simulation results indicate that: the slip ratio follows the optimum slip ratio, the input signal is smooth, achieve the purpose.

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Periodical:

Applied Mechanics and Materials (Volumes 336-338)

Pages:

973-977

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.336-338.973

Citation:

Cite this paper

Online since:

July 2013

Authors:

Long Fei Fu, Yu Ren Li, Guang Lai Tian, Bo Liang, Hong Ling Wang

Keywords:

Aircraft Anti-Skid Braking System, Index Reaching Law, Sliding Mode VSC, Slip Ratio

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