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导弹故障诊断系统减振器设计
引用本文:张伟,胡昌华,周涛,夏启兵. 导弹故障诊断系统减振器设计[J]. 导弹与航天运载技术, 2003, 0(1): 50-52
作者姓名:张伟  胡昌华  周涛  夏启兵
作者单位:第二炮兵工程学院,西安,710025
基金项目:国家教委高校骨干青年教师资助计划,国家自然科学基金重点课题 (代号 6993 10 40 )资助
摘    要:某导弹故障诊断系统减振器设计遵循隔振、缓冲系统期望的动态特性要求--变阻尼、变刚度,采用刚度拟合、干摩擦阻尼技术,实现了低固有频率、无谐振峰,并兼顾了缓冲要求。

关 键 词:故障诊断 减振器 动态特性
文章编号:1004-7182(2003)01-0050-03
修稿时间:2002-03-15

Design of the Shock Absorber in a Missile Fault Diagnosis System
Zhang Wei Hu Changhua Zhou Tao Xia Qibing. Design of the Shock Absorber in a Missile Fault Diagnosis System[J]. Missiles and Space Vehicles, 2003, 0(1): 50-52
Authors:Zhang Wei Hu Changhua Zhou Tao Xia Qibing
Abstract:Design of the shock absorber in a missile fault diagnosis system is based on its dynamic property, i.e. the shock absorber must adapt to the needs of variable damping and variable rigidities, hence, the technologies of rigidity approach and dry friction damp are applied to the design of the shock absorber. And the target of low-intrinsic-frequency and no-resonant peak has been achieved.
Keywords:Fault diagnosis  Shock absorber  Dynamic property
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