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舵回路是无人机飞行控制系统中的一个重要环节。飞行控制系统通过舵回路控制无人机的角运动,从而实现对无人机的操纵使其稳定飞行。基于某型号磁滞电机和“田口”三次设计方法,分析了位置反馈和速度反馈对舵回路的影响,确定了其取值范围,设计了某型号无人机舵回路,并进行了仿真试验,试验结果表明,该设计是可行的。
The rudder loop is an important part of the UAV flight control system. The flight control system controls the angular motion of the drone via the rudder loop, enabling the UAV to operate stably. Based on a certain type of hysteresis motor and “Taguchi” three times design method, the influence of position feedback and speed feedback on the rudder circuit is analyzed. The range of the rudder is determined. A certain type of UAV rudder circuit is designed and simulated The test results show that the design is feasible.