Pilot Induced Oscillation (PIO) was observed in the pilot control of the aircraft during some missions-landing and tochdown, up and away flight. This is considered the phenomenon of PIO is caused by the interference of pilot control and output of aircraft dynamic response. Therefor, the problems are found not only characteristics of the aircraft dynamic response but also pilot's manipulation to control the aircraft at the mission.
In this paper, it is shown the PIO have notable for bandwidth ω
BW≤1 (rad/s) of the closed loop and for such a condition of the system a lowering of the pilot gain and a leading of the phase lag is good method to suppress of the PIO tendency in manual control system.
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