Paper Title
Analysis And Design Of The Multiple Kalman Filter For Gyro Systems

Abstract
This paper presentsan adapt filter system to reduce the noise of gyro system of unmanned aerial vehicle. Radial basis function network and multiply Kalman filter are used with vector acceleration and angular acceleration. The gyro noise feature can be estimated to adjust numbers of Kalman filter layers. The proposed method can increase reliability of gyro data. Index Terms- Gyro, Radial basis function kernel, Kalman Filter.