MISSILES AND GUIDANCE TECHNOLOGY

A Simaplied SAGE-HUSA Kalman Filetering Algorithm

  • TIAN Hai ,
  • ZHU Xinyan
Expand
  • Automobile Management Institute of PLA, Anhui Bengbu 233011, China

Received date: 2009-10-28

  Online published: 2025-05-30

Abstract

Self-adaptive Kalman filtering algorithm was adopted in the online estimate of navigation state of unmanned aerial vehicle (UAV) because the simplified model is often used. At the moment, the algorithms usually applied in this territory are not perfect. Take the advantage of residue characteristics and choose the estimation windows, a simplified SAGE-HUSA Kalman filtering algorithm was given. The result of simulation shows this method agrees with the demand of engineering application of UAV.

Cite this article

TIAN Hai , ZHU Xinyan . A Simaplied SAGE-HUSA Kalman Filetering Algorithm[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(1) : 75 -77,84 . DOI: 10.15892/j.cnki.djzdxb.2011.01.005

References

[1]
Gerlach K. Outlier resistant adaptive matched filtering[J]. IEEE Transactions on Aerospace and Electronic Systems, 2002, 38(3): 885-901.
[2]
Qi Song, Zhe Jiang. Noise covariance identification based adaptive UKF with application to mobile robot systems[C]// IEEE International Conference on Robotics and Automation Roma, 2007: 4164-4169.
[3]
周露, 李东江, 闻新. 具有随机偏差的最优多段卡尔曼估值器[J]. 系统工程与电子技术, 2003, 25(7): 790-792.
[4]
沈云锋, 朱海, 莫军, 等. 简化的 Sage-Husa 自适应滤波算法在组合导航中的应用及仿真[J]. 青岛大学学报, 2001, 16(1): 44-48.
[5]
王社伟, 张洪钺, 陶军. 基于半马尔可夫过程的容错导航系统可靠性分析[J]. 航天控制, 2006, 24(2): 84-87.
Outlines

/