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In this paper, the dynamic system is analyzed by mathematical modeling, and a flight control system of the quadrotor unmanned aerial vehicle based on the hardware and software is studied and implemented. First, the dynamic model of the quadrotor unmanned aerial vehicle is constructed and analyzed theoretically; Second, the rack of the quadrotor unmanned aerial vehicle is designed, to test, analyze and experiment each component module;Third, a flight control system of the quadrotor unmanned aerial vehicle is realized by integrating software and hardware and conduct flight tests. Finally, the experimental results show that the flight control system of the quadrotor unmanned aerial vehicle of being implemented has achieved good flight control effect, with the advantages of strong sensitivity, high stability and excellent overall performance and so on.