Fault-tolerant Control for Semi-autonomous Damper
This paper studies the problem of designing adaptive fault-tolerant controller for semi-autonomous control aircraft landing gear,and the magneto-rheological damper is used as shock absorber of aircraft landing gear.The dampening system adjusts damping force to reduce aircraft landing impact load and oscillation frequency according to the real-time feedback to ground.When the plane lands,the plane often makes a big impact load,It is very easy to cause the damage of actuator unit and important for the safety of the aircraft.This paper uses H-infinity and fault-tolerant control to reduce influence of landing gear actuator fault and have ability of anti-disturbance,And good control effect can get from the simulation.
Landing gear MR fluid damper system fault-tolerant semi-autonomous control H-infinity control
Yi-bo Li Bin-Bin Gao Wei Guan
School of automation, Shenyang Aerospace University,110136
国际会议
the 25th Chinese Control and Decision Conference(第25届中国控制与决策会议)
贵阳
英文
623-628
2013-05-01（万方平台首次上网日期，不代表论文的发表时间）