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机载惯导系统减振设计
引用本文:宁月光,贾新强.机载惯导系统减振设计[J].现代导航,2015,6(6):497-501.
作者姓名:宁月光  贾新强
作者单位:海军装备部驻西安地区军事代表局,西安 710043
摘    要:为了保证机载惯导系统的性能和可靠性,减振系统的设计至关重要。本文根据机载惯导系统的使用环境,提出了系统对减振系统的要求,并针对平台式惯导系统和捷联惯导系统, 建立了相应的系统振动动力学模型。在总结减振系统设计指标的基础上,提出了机载惯导减振系统的设计方法,包括减振系统结构形式的选取、减振器材料和结构的确定、减振系统固有频率的确定以及阻尼特性设计等。按照设计方法,给出了一个平台惯导减振系统设计实例,该减振系统满足系统需要。

关 键 词:平台式惯导系统  减振系统  减振器

Damping Design of Airborne Inertial Navigation System
Authors:NING Yueguang  JIA Xinqiang
Abstract:Damping design is important for keeping the performance and reliability of airborne inertial navigation system. Under the environment of the airborne inertial navigation system, the requirement of damping system is presented in this paper, and the relevant dynamic model is set up according to the platform inertial navigation system and the strap-down inertial navigation system. The damping design of airborne inertial navigation system is presented, which includes choosing the structure of damping system, determining the material and structure of damper and the inherent frequency of damping system. According to the design method, a damping design of platform inertial navigation system is put forward and satisfied by the demands of this damping system.
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