摘要
本文研究微机械陀螺仪及其在炮射导弹瞬时飞行姿态测量中的应用。文中介绍了微机械陀螺仪的工作原理、数学模型及其应用系统。该陀螺仪采用硅微机械加工技术制造，体积小，便于装入弹体内，可实时测量炮射导弹俯仰、偏航和滚转三种运动姿态。
This paper studied on micromechanical gyros and its application on gun-launched missile attitude determination. The micromechanical gyros, works principle, methematics model and measurement system was introduced. Because the micromechanical gyros was fabricated by IC manufacture technology, it has micro volume, and can be easily enclosed into missile body. The system can detect axis, radial and roll attitude angles of the gun-launched missile in realtime.
出处
《电子测量与仪器学报》
CSCD
1999年第2期30-34,共5页
Journal of Electronic Measurement and Instrumentation
基金
国家杰出青年基金!59725512
省自然科学基金!981023
关键词
微机械陀螺仪
导弹
姿态测量
Micromechanical gyros
Missile
Attitude dertermination
