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导弹发射车主动控制悬架多ェ况减振研究
引用本文:徐伟国,毕世华,陈阵.导弹发射车主动控制悬架多ェ况减振研究[J].兵工学报,2007,28(8):909-914.
作者姓名:徐伟国  毕世华  陈阵
作者单位:北京理工大学机电工程学院,北京100081
摘    要:某车载导弹武器系统拟采用任意点无支撑发射方式,采用主动控制悬架可以使运输发射车重要部位同时满足导弹发射和机动状态的减振要求。对于发射和机动两种工况,分别应用最优控制和自适应控制理论设计控制器,并给出了作动器的切换策略。仿真计算显示该方法有较好的减振效果。

关 键 词:自动控制技术      兵器发射理论与技术      导弹运输发射车      发射冲击激励      随机路面激励      振动的主动控制      模糊控制  
文章编号:1000-1093(2007)08-0909-06
修稿时间:2005-10-08

Research on Vibration Damping for Missile Launcher with Active Suspensions Under Multiple-loading Case
XU Wei-guo,BI Shi-hua,CHEN Zhen.Research on Vibration Damping for Missile Launcher with Active Suspensions Under Multiple-loading Case[J].Acta Armamentarii,2007,28(8):909-914.
Authors:XU Wei-guo  BI Shi-hua  CHEN Zhen
Affiliation:School of Mechatronic Engineering, Beijing Institute of Technology, Beijing 100081, China
Abstract:An arbitrary-site support-free launching mode is intended to be taken by some vehicular missile weapon system. The vibration damping requirements of the key section of missile transporter-launcher can be met by using active suspensions for both the launching and maneuvering states simultaneously. By using optimal control and adaptive control theoryies respectively, two controllers were designed for launching and maneuvering states and the actuator switching strategy was also given. The simulation results prove that the method has a satisfactory vibration damping effect.
Keywords:automatic control technique  weapon launching theory and technology  missile transporter-launcher  launching shock excitation  random road excitation  active control of vibration  fuzzy control
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