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两轴地磁信号修正的陀螺姿态算法
引用本文:苑大威,曹红松,王泉,杜韩东.两轴地磁信号修正的陀螺姿态算法[J].弹箭与制导学报,2010,30(5).
作者姓名:苑大威  曹红松  王泉  杜韩东
作者单位:中北大学弹箭模拟仿真研究中心,太原,030051
摘    要:目前捷联式惯导系统是惯性技术的发展方向,姿态算法是捷联惯导系统算法中的一个重要组成部分,其精度直接影响弹体姿态控制能力,为此文中提出了一种采用三轴MEMS陀螺进行姿态探测,并用两轴地磁信号解算出的滚转角修正陀螺累计误差的方案,仿真分析了地磁陀螺信号组合测姿算法。结果表明:该方案相对于单纯陀螺信号解算姿态角精度高,可用于改善测姿结果。

关 键 词:MEMS陀螺  磁强计  四元数  旋转矢量  

The Gyro Attitude Algorithm of Two-axis Geomagnetic Signal Correction
YUAN Dawei,CAO Hongsong,WANG Quan,DU Handong.The Gyro Attitude Algorithm of Two-axis Geomagnetic Signal Correction[J].Journal of Projectiles Rockets Missiles and Guidance,2010,30(5).
Authors:YUAN Dawei  CAO Hongsong  WANG Quan  DU Handong
Affiliation:YUAN Dawei,CAO Hongsong,WANG Quan,DU H,ong(Research Center of Projectiles , Rockets Analog Simulation,North University of China,Taiyuan 030051,China)
Abstract:Presently,the strapdown inertial system has become one of the most important research directions of inertial technology,attitude algorithm is an important part of SINS algorithm,and the algorithm's accuracy will directly affect attitude control.In this paper,the scheme which adopts three-axis MEMS gyro for attitude detection and rolling angles resolved by two-axis magnetometer signals for gyro accumulative error correction was proposed.The algorithm of gyro and magnetometer calculating missile's attitude wa...
Keywords:MEMS gyro  magnetometer  quaternion  rotation vector  
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