摘要
采用四元数算法对微惯性航向、姿态系统进行姿态解算。在实验室进行的大量实验表明,温度对系统性能有很大影响,对陀螺零点偏置的温度补偿进行了分析研究,实验结果表明补偿对系统稳定性起到了很好的作用。
The paper is about calculating the attitude of the objects by quaternion in the micro heading and attitude system. Numerous about the stability. Key words experiments carried in laboratory indicate that temperature has affected the system capability. This paper has a research temperature compensation to gyroscopic zero-bias and the result is that compensation has good effect on the system stability.
出处
《机械工程与自动化》
2006年第3期115-117,共3页
Mechanical Engineering & Automation
关键词
硅微陀螺
惯性测量
温度补偿
micro silicon-gyro
inertial measurement
temperature compensation
