空基激光陀螺捷联惯导系统导航精度的分析与研究  

Analysis and Study on Navigation Accuracy of Laser Gyro SINS System of Vacuous Basis

作　　者：岳明桥[1] 李高鹏[1] 

机构地区：[1]92941部队

出　　处：《战术导弹技术》2005年第4期40-42,65,共4页Tactical Missile Technology

摘　　要：从现代导弹的实际情况出发,通过对空基激光陀螺捷联惯导系统导航工作原理的分析,总结了空基激光陀螺捷联惯导系统导航误差产生的原因,归纳了激光陀螺和加速度计的误差模型和补偿.Going from the practical situation of modern missile, the operation theory of laser gyro SINS system of vacuous basis is analyzed. The generated reasons of navigation error of laser gyro SINS system of vacuous basis are summarized. The error model and compensation of laser gyro and acceleration are generalized.

关 键 词：捷联惯导 惯性导航 激光陀螺 加速度计 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]