Muti-wheel Bogie Braking System Simulation of Civil Aircraft
Hua-wei Wu, Te-fang Chen, Lin-feng Wang, Wei-ming Huang
Available Online November 2012.
- https://doi.org/10.2991/citcs.2012.116How to use a DOI?
- bogie; muti-wheel; Simulation; braking system; slip-ratio
- 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.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
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 - 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 - https://doi.org/10.2991/citcs.2012.116 ID - Wu2012/11 ER -