PID Controller Design and Numeric Simulation on Aircraft Arresting System

摘要

The control principle of aircraft arresting system was introduced in this paper. And taking the wire rope hydraulic aircraft arresting system as research object, deduced the transfer function model of the system by using the method of linearization. At the same time, the optimized PID controller based on the control goal of constant acceleration was designed. Then apply the controller to the control of aircraft arresting system. The simulation result indicated that the control system applied this controller possessed all right arresting effect, so aircraft arresting system can be applied to most types of aircraft.