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The anti-jamming attitude control system of the four-rotor UAV currently designed has poor anti-jamming capability and poor control performance. In order to solve the above problems, a new anti-jamming attitude control system for quad-rotor UAV was designed based on hybrid filtering, and the hardware and software of the system were optimized. The system hardware mainly includes the main controller, sensor module, motor drive control module, wireless data transmission module, etc. The collected attitude and position information of quadrotor UAV needs to be solved by the master controller. According to the air target flight mission, the attitude control algorithm is used to control the motor speed by using the output PWM wave signal, so as to realize the control of quadrotor UAV's flying attitude and hovering position. The hardware system integrates dual gyroscope and dual acceleration structure. Acceleration structure. The software control process is realized through system initialization, determination of flight attitude angle, and input of attitude control algorithm. The experimental results show that the anti-jamming attitude control system based on hybrid filter has strong anti-jamming ability, high control ability and fast response speed.