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.