基于磁滞电机的无人机舵回路设计  

Design for Rudder Circuit of UAV Based on the Hysteresis Motors

作　　者：陈峰[1] 

机构地区：[1]中国人民解放军92419部队

出　　处：《宇航计测技术》2015年第4期48-53,共6页Journal of Astronautic Metrology and Measurement

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。Rudder circuit is an important part of flight control system of UAV （ unmanned aerial ve- hicle）. Flight control system could control the angle motion of UAV via the rudder circuit, in order to a- chieve 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 deter-mined, a certain type of UAV rudder circuit is designed. The test results of simulation experiment show that the design is feasible.

关 键 词：无人机 磁滞电机 舵回路 

分 类 号：V279.1[航空宇航科学与技术—飞行器设计]