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Abstract: There will be a great impact load on the arresting system when the carrier aircraft landing the ship, and the risk is extremely high. the characteristics of the aircraft arresting system must be estimated. The establishment of a large non-standard test stand for arresting system of the carrier aircraft is an important method to verify the characteristics of aircraft arresting system. In order to solve the problem of motor driving in the former test stand, hydraulic pump station and hydraulic accumulator are used in this design. The problem of measuring and controlling of high speed hydraulic cylinder is solved. In this system, the RTOS(Real Time Operating system)、 the mode of host computer and slave computer and the programming language of Labview are used to realize the high-speed motion control of the hydraulic cylinder. The stability control of hydraulic cylinder under large speed and load is realized. The system is designed to apply a continuous adjustable loading force from 0KN to 90KN, continuously adjustable sliding speed from 0 m/s to 9m/s, and continuously adjustable angle from 100°～180°.The test results can provide data support for the evaluation of the characteristics of aircraft arresting system.