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基于磁滞电机的无人机舵回路设计CSCD
引用本文:陈峰.基于磁滞电机的无人机舵回路设计CSCD[J].宇航计测技术,2015,35(4):48-53.
作者姓名:陈峰
作者单位:1、中国人民解放军92419部队,辽宁 125106
摘    要: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。

关 键 词:无人机  磁滞电机  舵回路  UAV  Hysteresis  motors  Rudder  circuit

Design for Rudder Circuit of UAV Based on the Hysteresis Motors
CHEN Feng.Design for Rudder Circuit of UAV Based on the Hysteresis Motors[J].Journal of Astronautic Metrology and Measurement,2015,35(4):48-53.
Authors:CHEN Feng
Institution:1、92419 Unit of PLA, Liaoning 125106
Abstract:Rudder circuit is an important part of flight control system of UAV(unmanned aerial vehicle).Flight control system could control the angle motion of UAV via the rudder circuit,in order to achieve its stable flight.Based on a model of hysteresis motors and "Taguchi" three design methods, the effect on the rudder circuit by feedback of position and velocity is analyzed, its value range is determined, a certain type of UAV rudder circuit is designed.The test results of simulation experiment show that the design is feasible.
Keywords:UAV                                                                                                                        Hysteresis motors                                                                                                                        Rudder circuit
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