某型导弹气动舵机稳态误差不稳定原因分析  

Pneumatic Actuator Steady State Error Unstable Reason Analysis of Certain Type Missile

作　　者：肖精华 张海波 

机构地区：[1]总装武汉军代局驻长沙地区军事代表室,长沙411207

出　　处：《兵工自动化》2014年第10期60-62,共3页Ordnance Industry Automation

摘　　要：针对某型导弹气动舵机在线返修率较高的情况,对舵机稳态误差不稳定机理进行分析。简要介绍舵机的结构、特点及各部件的功能,分解检查故障产品,逐项排查生产过程,找出造成舵机稳态误差不稳定的原因。在此基础上有针对性地提出相应措施。结果表明:采用该方法使舵机的稳态误差不稳定现象得到显著改善,确保了后续产品的质量。Aiming at a certain type of missile aerodynamic online repair rate is high, analyzed the steady state error ofinstability mechanism. Briefed the structure, characteristics of steering gear and the function of each part, decompositionfailure to check the product production process, one by one investigation, find out the cause of the steady-state error is notstable. On this basis, put forwards the corresponding measures. The results show that, using this method to make the stateerror the unstable phenomenon has been significantly

关 键 词：舵机 故障 电磁铁 措施 

分 类 号：TJ765.4[兵器科学与技术—武器系统与运用工程]