摘要
将数据融合方法引入到导弹制导系统 ,充分利用余度捷联惯性测量装置中多陀螺的重复测量信息提高导弹的制导精度。数据融合过程分为两步 :首先应用分布图对传感器原始数据进行一致性检测 。
The data fusion method is applied to guidance system of the missile in this paper. The redundant data with a stochastic noise from different gyroscopes in the redundant strapdown IMU is fully exploited and guidance precision of the missile is increased. Data fusion process is divided into two steps. We can obtain the consistent sensor data using the distribution display method, then consensus multisensor data is fused with parameter estimation method.
出处
《计算机自动测量与控制》
CSCD
2001年第6期12-13,16,共3页
Computer Automated Measurement & Control
