Muti-wheel Bogie Braking System Simulation of Civil Aircraft

DOI

10.2991/citcs.2012.116How to use a DOI?

Keywords

bogie; muti-wheel; Simulation; braking system; slip-ratio

Abstract

In order to meet the development needs of large civil aircraft, this paper takes four-wheel bogie landing gear as example and introduces the muti-wheel braking system control mode and control law. The kinematics of aircraft braking process and the mathematical models of wheels, tyres and runway, hydraulic servo valves, brakes, etc. are analyzed. Yaw movement is introduced on the basis of the original three degrees of freedom movement. The multi-wheel simulation system based on fuzzy control with "I" mode is established. Five common landing states of muti-wheel aircraft are simulated, results show the control parameters are real-time adjust to make full use of runway friction force, the overall braking effect is desirable. Thus it provides an insightful new way of thinking for successful development of multi-wheel bogie aircraft braking system in integrated environment.

Copyright

© 2012, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Hua-wei Wu
AU  - Te-fang Chen
AU  - Lin-feng Wang
AU  - Wei-ming Huang
PY  - 2012/11
DA  - 2012/11
TI  - Muti-wheel Bogie Braking System Simulation of Civil Aircraft
BT  - Proceedings of the 2012 National Conference on Information Technology and Computer Science
PB  - Atlantis Press
SP  - 449
EP  - 453
SN  - 1951-6851
UR  - https://doi.org/10.2991/citcs.2012.116
DO  - 10.2991/citcs.2012.116
ID  - Wu2012/11
ER  -