摘要
本文为提高制导精度,讨论了用于惯性平台的连续瞄准、校准的卡尔曼滤波器,介绍平台系统和加速度表的误差模型、参数辨识的卡尔曼滤波方法及重力残数加速度表校准原理。
In this paper, in order to raise the guidance accuracy, a kalman filter for con-
tinuous alignment and calibration of the inertial platform is described. Then introdace the er-
rors model of a platform system and accelerometer, Kalman filtering methods for paramatric
identification and the calibration principle of gravity measurement residue of accelerometr.
出处
《航天控制》
CSCD
北大核心
1992年第4期28-40,共13页
Aerospace Control
关键词
制导
卡尔曼滤波
校准
Guidance
Kalman filter
Alignment
Calibration