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阻尼状态下捷联惯导系统组合导航方法探讨
引用本文:刘玉祝,郑辛,李群.阻尼状态下捷联惯导系统组合导航方法探讨[J].战术导弹控制技术,2009(3):13-16.
作者姓名:刘玉祝  郑辛  李群
作者单位:北京自动化控制设备研究所,北京100074
摘    要:惯性导航系统在干扰量的作用下,会产生周期性的振荡误差及随时间积累的误差。引入阻尼网络可以对系统振荡误差进行阻尼。而利用外界位置或速度信息则可以修正随时间积累的误差。选择合适的阻尼网络,建立阻尼状态下系统的误差方程,是对长航时激光捷联惯导系统在阻尼状态下的组合导航方法进行分析的基础。计算机仿真和工程试验结果表明:与无阻尼时的导航结果相比,该方法能够一定程度上抑制误差的振荡和随时间的积累,提高了系统的精度。

关 键 词:惯性系统  水平阻尼  组合导航

Integrated navigation method of strapdown inertial navigation system under damping condition
LIU Yu-zhu,ZHENG Xin,LI Qun.Integrated navigation method of strapdown inertial navigation system under damping condition[J].Control Technology of Tactical Missile,2009(3):13-16.
Authors:LIU Yu-zhu  ZHENG Xin  LI Qun
Affiliation:LIU Yu-zhu,ZHENG Xin,LI Qun (Beijing Institute of Automatic Control Equipment,Beijing 100074,China)
Abstract:Inertial navigation system can have periodic vibration error which caused by disturbance quantity. The error also accumulates along with time. The damping network can affect system vibration error. Using outside position or speed information may revise the error that accumulates along with time. Selecting suitable damping network and analyzing the system error equation under damping condition are the first steps to research integrated navigation method while the SINS works for long time under damping condit...
Keywords:inertial navigation system  horizontal damping  integrated navigation system  
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