Maximum Correntropy Unscented Kalman Filter for Ballistic Missile Navigation System based on SINS/CNS Deeply Integrated Mode

Maximum Correntropy Unscented Kalman Filter for Ballistic Missile Navigation System based on SINS/CNS Deeply Integrated Mode

Strap-down inertial navigation system/celestial navigation system (SINS/CNS) integrated navigation is a high precision navigation technique for ballistic missiles. The traditional navigation method has a divergence in the position error. A deeply integrated mode for SINS/CNS navigation system is pro...

Full description

Bibliographic Details
Main Authors: Bowen Hou, Zhangming He, Dong Li, Haiyin Zhou, Jiongqi Wang
Format: Article
Language:English
Published: MDPI AG 2018-05-01
Series:Sensors
Subjects:
unscented Kalman filter
maximum correntropy
SINS/CNS deeply integrated navigation
non-Gaussian noises
ballistic missile
Online Access:http://www.mdpi.com/1424-8220/18/6/1724

Internet

http://www.mdpi.com/1424-8220/18/6/1724

Similar Items