摘要
初步总结了研制的 YT-1型液浮速率积分陀螺进行的漂移随机模型试验,为卫星的姿控系统提供实时控制的随机数学模型。
This paper is a preliminary summary for the floated rate integra-tion gyro developed by Beijing Institute of Control Engineering.Its aim is tooffer a random mathematical model of the drift process for the attitudecontrol system of a satellite.This paper analyses gyro's data got in testwith the method of time series analysis.The conclusion is that the randommodel of the gyro can be expressed similar to a first order auto-regressionmodel in general.
出处
《中国空间科学技术》
EI
CSCD
北大核心
1990年第5期24-30,共7页
Chinese Space Science and Technology
关键词
卫星
陀螺
姿态控制
随机模型
漂移
Subject Term Satellite
Gyro error model
Attitude control
Drift.
