High-efficiency aircraft antiskid brake control algorithm via runway condition identification based on an on-off valve array

Author:

SUN DongORCID,JIAO Zongxia,SHANG Yaoxing,WU Shuai,LIU Xiaochao

Funder

National Nature Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference35 articles.

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2. Hydraulic piston pump in civil aircraft: Current status, future directions and critical technologies;Guo;Chin J Aeronaut,2020

3. Experimental based analysis of the pressure control characteristics of an oil hydraulic three-way on/off solenoid valve controlled by PWM signal;Jeong;J Dyn Syst, Meas, Control,2002

4. Stubbs SM, Tanner JA, Smith EG. Behavior of aircraft antiskid braking systems on dry and wet runway surfaces. a slip-velocity-controlled, pressure-bias-modulated system. NASA Langley Research Center, Hampton; 1979. NASA TP-1051.

5. Aircraft antilock brake system with neural networks and fuzzy logic;Tseng;J Guidance Control Dyn,1995

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