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无陀螺捷联惯导系统模型研究
引用本文:汪小娜,王树宗,朱华兵.无陀螺捷联惯导系统模型研究[J].兵工学报,2006,27(2):288-292.
作者姓名:汪小娜  王树宗  朱华兵
作者单位:海军工程大学,兵器工程系,湖北,武汉,430033;海军工程大学,兵器工程系,湖北,武汉,430033;海军工程大学,兵器工程系,湖北,武汉,430033
摘    要:无陀螺捷联惯导系统采用加速度计来解算载体相对惯性系的角速度,从而代替角速度陀螺仪。考虑重力影响,对两种不同配置方式的6加速度计捷联惯导系统建立了载体运动参数解算模型,在此基础上提出了一种12加速度计配置方式,从而利用多传感器的冗余信息对算法进行优化,消除了角速度解算过程中求解微分方程带来的累积误差,提高了角速度解算精度。

关 键 词:飞行器控制、导航技术  无陀螺  捷联惯导  加速度计  配置
文章编号:1000-1093(2006)02-0288-05
收稿时间:2004-09-23
修稿时间:2004-09-23

Study on Models of Gyroscope-free Strap-down Inertial Navigation System
WANG Xiao-na,WANG Shu-zong,ZHU Hua-bing.Study on Models of Gyroscope-free Strap-down Inertial Navigation System[J].Acta Armamentarii,2006,27(2):288-292.
Authors:WANG Xiao-na  WANG Shu-zong  ZHU Hua-bing
Affiliation:Department of Weaponry Engineering, Naval University of Engineering, Wuhan 430033,Hubei, China
Abstract:The angular velocity was computed using accelerometers instead of angular velocity gyroscopes in gyroscope-free strap-down inertial navigation system(GFSINS).The models for computing the parameters about the carrier motion of two kinds of 6-accelerometer configuration GFSINS schemes were established under considering gravitational effect.Based on this,a 12-accelerometer configuration scheme was proposed.The algorithm is optimized using the sensor redundant information and the accumulative error deriving from the solution of differential equations is reduced and the accuracy of the computed angular velocity is increased.
Keywords:control and navigation for fligh vehicle  gyroscope-free  strap-down inertial navigation  accelerometer  configuration
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